. .9. ml... u .1 .. ,1.) $32 Nth... two ‘ IN! . . fin, LI . 0 WP. . I $ ”a. “ L33: ‘ Emma ”MM 2. a. 33.4 £3. . I ‘2 5 1:. . I! I“ c .. .5 . ”$5”?me ; . .r..h.£fi.mwfl1swa 8.41.43 5... .‘glkwawm hfiqumuzflm... hflwnéh 7rd... . A11; 17131». v {a I .. a. . a, »X) 11 13': all". , t\ if. 1 xi :‘AFJCD'7 .UBRARY MlChIg. .i State University This is to certify that the thesis entitled PERFORMANCE PROPERTIES OF A BIODEGRADABLE FOAM (GFIREN CELL®) FOR PACKAGING APPLICATIONS presented by Samina Arif has been accepted towards fulfillment of the requirements for the Master of degree in Packaging Science 7 Major Profe'ssor’s Signature & 7/2 5/0 7 Date MSU is an affirmative-action, equal-opportunity employer -.-.-.-.-.-u---------o-.—.---— -n-.-.--v--------.- -.-.-.-.-.-.-.-.-.-.- -------o-o---n--o- PLACE IN RETURN BOX to remove this checkout from your record. To AVOID FINES return on or before date due. MAY BE RECALLED with earlier due date if requested. DATE DUE DATE DUE DATE DUE 6/07 p:lCIRC/DateDue.indd-p.1 PERFORMANCE PROPERTIES OF A BIODEGRADABLE FOAM (GREEN CELL®) FOR PACKAGING APPLICATIONS. By Samina Arif A THESIS Submitted to Michigan State University In partial fulfillment of the requirements For the degree of MASTER OF SCIENCE The School of Packaging 2007 ABSTRACT PERFORMANCE PROPERTIES OF A BIODEGRADABLE FOAM (GREEN CELL®) FOR PACKAGING APPLICATIONS By Samina Arif Green Cell® foam is a biodegradable foam packaging material produced from a proprietary cornstarch blend. It is commercially available in a variety of laminations and constructions. Cushioning ability and thermal resistance (R- value) are fundamental properties needed to compete against synthetics. Since Green Cell® foam is starch based and biodegradable, moisture is likely to affect its physical properties. Cushioning characteristics and the R- values of 1 and 2-inch foams were determined as a function of temperature and moisture content. ASTM method 1596 was used to determine the cushioning properties and an ice melt method was used to determine thermal resistance. Moisture sorption isotherms were developed at three temperatures (20°C, 25°C and 30°C) to determine its moisture sensitivity. One-inch foam had a lower G value at lower static stress than synthetic foams, but at higher static stress had higher G values, while two-inch foam had G values similar to that of synthetic foam materials. Dimensional changes were observed at higher relative humidity conditions especially at 30°C. The R-values at higher humidity were also less than that of synthetic materials. Biodegradable Packaging materials will find niche markets, as long as their properties are comparable to synthetic materials. Green Cell® foam’s hygroscopicity and its density need to be more controllable, then this would open the door for new market opportunities for this biodegradable foam manufactured from renewable resources. In the near, the farm may make a significant in the area of biobased Packaging Materials. Dedicated to my dear husband and son iii \\ iii. If "’9. in SC ACKNOWLEDGEMENTS Words seem inadequate to express my feelings of gratitude, however, I would like to thank Dr. Bruce Harte, Professor, The School of Packaging, MSU, East Lansing, Michigan, for his continuous and substantive contributions during all phases of this project. I, further, gratefully acknowledge all of his efforts and contributions to present our research in two International proceedings (annual IFT conference2005, and 4th International Biomechanics conference2003). I extend my gratitude to Dr. Burgess for his insightful comments and very valuable suggestions during our two poster presentations, master thesis writing and during all phases of this Research. Special appreciation to Dr. Ramani Narayan for serving on my guidance committee. Thanks to all of my friends and teachers in the School of Packaging especially Dr. Rafael Auras, providing the valuable information during my research when I was stuck. I further would like to acknowledge to my Schoolfellow Krittika, Tanprasert (Kate) giving her valuable time to help us to get our poster (Evaluation of biodegradable foam for packaging applications) into the final shape when I was physically away from my school. Last but definitely not least; I would like to thank my family (husband and son) during my very busy years of the school. My young son “Ibrahim Arif” could always cheer me up even on the worst of the days and my husband who always kept me pushing forward. iv fisxrsfigsi‘ TABLE OF CONTENTS INTRODUCTION .................................................................................... 1 CHAPTER 1 ................................................................................... 4 1.0 Literature review .............. . ................................................................ 4 1 . 1 Introduction .................................................................................... 4 1.2 History ......................................................................................... 5 1.21 Early History ................................................................................. 5 1.22 1800’s .......................................................................................... 5 1.23 1900’s .......................................................................................... 6 1.24 1920’s .......................................................................................... 6 1.25 1960’s .......................................................................................... 7 1.26 2000 and Beyond ........................................................................... 7 1.30 History of Plastic Foam .................................................................... 8 1.31 .Early History (2680-2565 BC) ............................................................ 8 1.32 1000-1500 History ........................................................................... 9 1.33 1887 History ................................................................................ 10 1.40 Biodegradability ........................................................................... 1 1 1.41 Key Elements in Biodegradation ......................................................... 12 1.42 Bioplastics ................................................................................... 14 1.42.1 Starch ........................................................................................ 15 1 .43 Retrogradation .............................................................................. 16 1.43.1 Retrogradation process of starch ......................................................... 17 1.44 Thermal Insulation .......................................................................... 19 1.45 Green Cell® Foam ......................................................................... 22 1.45.1 Composition of Green Cell® foam ...................................................... 22 1.46 Foam Definition ............................................................................ 22 1.47 Types of Commercial Foam .............................................................. 23 1.47.1 Polystyrene foam .......................................................................... 25 1.47.2 Polyurethane Foam ........................................................................ 31 1.47.3 Polyolefin foam ............................................................................ 39 1.50 Manufacturing methods for Plastic Foams ............................................. 42 1.51 Injection molding .......................................................................... 42 1.52 Extrusion .................................................................................... 44 1.53 Other Processes ............................................................................ 47 CHAPTER 2 ......................................................................................... 50 2.0 Twin Screw Extrusion process ............................................................ 50 2.1 Cushioning Characteristics of Green Cell® Foam .................................... 53 2.1 1 Instrumentation ............................................................................. 53 2.12 Method ....................................................................................... 54 ......a-.. a. 3.. 1.1.. 1.. .......... 4. 4. 4. 2.13 Calculations .................................................................................. 55 2.14 Effect of % RH and temperature on G values ........................................... 56 2.15 Effect of Time on G values ................................................................ 57 2.2 Dimensional Changes ...................................................................... 58 Materials .................................................................................... 58 Methods ..................................................................................... 59 Dimensional changes at different relative humidity (%RH) conditions and 30°C ......................................................................................... 59 Material behavior at ambient conditions ................................................ 60 The Change in thickness of Green Cell Foam under Specific load ............... 60 2.3 Sorption isotherm .......................................................................... 61 2.31 To determine the moisture sorption isotherm of the product at 20°C, 25°C 30°C .......................................................................................... 61 2.32 Net weight changes ......................................................................... 63 2.40 The package insulating ability (R -Value) and bulk density of Green Cell® foam ......................................................................................... 64 2.41 Materials .................................................................................... 64 Methods ..................................................................................... 65 Research Over view ....................................................................... 69 CHAPTER 3 ........................................................................................ 70 Results and Discussion .................................................................... 70 3.1 Cushioning characteristics of Green Cell Foam , G value at 25°C and 50%RH and comparison of values ............................................................... 71 3.11 Time Effect on G values ............................................................... 78 3.12 Effect of relative humidity on G value ................................................. 79 3.20 Dimensional stability .................................................................... 87 3.21 Material behavior at ambient conditions ................................................ 93 3.22 Changes in thickness under load ......................................................... 95 3.23 Change in Thickness under load at ambient conditions .............................. 98 3.30 Moisture sorption ......................................................................... 100 3.4 Thermal insulation ....................................................................... 1 15 4.0 CHAPTER 4 .............................................................................. l 19 4.1 Conclusion ................................................................................ 1 19 4.2 Recommendations ........................................................................ 120 vi APPENDIX -A .................................................................................... . 121 Cushioning Characteristics ....................................................... 121-139 APPENDIX- B ..................................................................................... 140 Dimensional Changes and Moisture gain/loss with respect to time at 11% RH and 30°C ........................................................................ 140-174 APPENDIX- C .................................................................................... 175 Moisture Sensitivity of Green Cell® Foam ...................................... 175-196 APPENDD(- D ..................................................................................... 197 Thermal insulation properties calculations of Green Cell® foam ............ 197-199 APPENDIX- E .................................................................................... 200 Standards Salt Solution preparation ............................................. 200-202 References .................................................................................... 204-207 vii LIST OF TABLES Table 1. Table No.1. Major types of commercial plastic foam ..................... 23 Table 2. Typical Fragility Levels for Different Products ............................. 72 Table 3. Comparison of G value of Green Cell Foam® 2— inch thick with the G values of other materials in the market.* (2” thickness,24 in Drop height) ..................................................................... 74 Table 4. Comparison of G value of *Green Cell® foam with the G values of other Commercial materials. (* 1” thickness 24” Drop Height). 77 Table 5. Comparison of G value of *GCF with respect to time Cell (Thickness 1- inch Green foam) ............................................. 79 Table 6. G value and change in weight (Aw) of Green Cell® foam with respect to time. .............................................................. 80 Table 7: Comparison of impact time and impact velocity before and after keeping the material at specific %RH conditions .......................... 81 Table 8. Relationship between change in Thickness under load at 25°C and 50% RH .............................................................. 95 Table 9. Relationship between change in Thickness under load at 25°C and 50% RH(* 2-inch Green Cell® foam) ................................. 96 Table 10. Relationship between change(A) .in Thickness at ambient conditions (* 2-inch Green Cell® foam) .............................................. 98 Table 11. R-values of EPS cooler and Green Cell cooler at different conditions .......................................................... 118 Tables Gl- G 7 Represent the information about the shock characteristics of Green Cell® foam having thickness of 2- inch ............................. 121-124 Tables G 8 to Gl6.Represent the information about the shock characteristics of Green Cell® foam having thickness of 2- inch ............................. 125-129 Table G17. Shock characteristic information before storing at different humidity viii conditions and 30°C ......................................................... 130 Table G18. Shock characteristic information after the storage study at different humidity conditions at 30°C ............................................. 130 Table G19 (a, b and c). Comparison of shock characteristics of Green Cell® foam before the storage studyand after the storage study at different relative humidity (%RH) conditions and 30°C .................................... 131 Table G 20. Comparison of G values of Green Cell® foam at different relative humidities with respect to time ............................................. 132 Table G 21-G23. Represent the information about the shock characteristics of Green Cell® foam having thickness of 2- inch with respect to time . . ...133-134 Table G 24-G27. Represent the information about the shock characteristics of Green Cell® foam having thickness of 1- inch with respect to time . . ...135-136 Table D l — D3. Dimensional Changes and Moisture gain/loss with respect to time at 11% RH and 30°C ...................................................... 140-141 Table D 4 mensional Changes and Moisture gain/loss with respect to time at 43% RH and 30°C ........................................................ 143-144 Table D 5-D8 Net Dimensional changes and weight loss/gain at 43% RH and 30°C ............................................................... 145-146 Table D 9 — D13. Dimensional Changes and Moisture gain/loss with respect to time at 56% RH and 30°C ........................................................ 148-151 Table D 14 — D18. Dimensional Changes and Moisture gain/loss with respect to time at 75% RH and 30°C ........................................................ 153-156 Table D 19 — D23. Dimensional Changes and Moisture gain/loss with respect to time at 84% RH and 30°C ........................................................ 159-163 Table D 24 — D 28. Dimensional Changes and Moisture gain/loss with respect to time at 89% RH and 30°C ........................................................ 165-168 Table D 29 — D 33. Dimensional Changes and Moisture gain/loss with respect to time at 95% RH and 30°C ........................................................ 170-173 Table M . Initial moisture Content Calculations of Green Cell® foam ........... 175 Table M 1. ‘ Experimental Moisture Content “Me” Calculations at 20°C and different humidity conditions ................................................... 176-181 ix Ta Table M 2. RMS calculation for GAB model at 20°C and different %RH conditions ....................................................................... 1 82 Table M 3. Experimental Moisture Content “Me” Calculations at 25°C and different humidity conditions .................................................. 183-188 Table M 4. RMS calculation for GAB model at 25°C and different %RH conditions ...................................................................... l 89 Table M 5. Experimental Moisture Content “Me” Calculations at 30°C and different humidity conditions ..................................................... 190-195 Table M 6. RMS calculations at 30°C and different %RH conditions ............... 196 Table T 1. (R-Value ) calculation of GCF and EPS coolers at 50%RH and 25°C. ........................................................................... 197-198 Table T 2. (R-Value ) calculation of GCF and EPS coolers at 80%RH and 30°C ........................................................................... 198-199 Table T 3. Density calculation of l-inchand 2-inch Green Cell® foam ........ 199 Table S-l; Equilibrium Relative humidity values (standards and actual) for selected saturated solutions ............................................................... 202 LIST OF FIGURES Figure 1. Historic pyramids (2680-2565 BC) ............................................... 8 Figure 2. Easter island (1000-1500) ......................................................... .9 Figure 3. Statue of Liberty (1887) ........................................................... 10 Figure 4. Schematic diagram for biodegradation of polymers ............................ 11 Figure 5. Key elements for biodegradation process ....................................... 13 Figure 6 Shows the Plastic foam basic structure of Starch molecule .................... 15 Figure 7 —10 Examples of Green Cell® Foam practical usage ............................ 21 Figure 11. Major types of foam materials and their applications ........................... 24 Figure 12. Basic structure of polystyrene .................................................... 30 Figure 13. Basic diagram of Extruder machine ............................................... 47 Figure 14. Process Flow Diagram of Green Cell® Foam .................................... 52 Figure 15. Overall Research overview of the Performance properties of Green Cell Foam ..................................................................... 69 Figure 16. Material damage at 1.75psi ,determine G value ,1“ impact .................... 74 Figure 17. G values of Green Cell® foam Vs Static Stress (psi) * 2-inch thick GCF .................................................................................... 75 Figure 18. Comparison of the G value of the GCF with the G values of other materials in the market available material. * (2” thickness 24” Drop Height) ......... 76 Fig19. Graphical representation of the G value of ‘Green Cell® foam with the G values of other commercial materials. *(l” thickness 24” Drop Height). . ...77 Figure 20. Graph between G values of GCF Vs Static stress (* l-inch thick GCF). 78 Figure 21. (Front view) Comparison of Green Cell® foam kept at 25°C, 50%RH and 30°C, 75% RH ........................................................................ 81 Figure 22 (Side view) Comparison of Green Cell® foam kept at 25°C, 50%RH and xi 30°C, 75% RH ........................................................................ 82 Figure 23. (Side view) Comparison of Green Cell® foam kept at 25°C, 50%RH and 30°C, 84% RH ...................................................................... .82 Figure 24. Material kept at 84% RH and 30°C ............................................... 83 Figure 25. (Front View) Comparison of Green Cell® foam kept at 25°C, 50%RH and 30°C, 89% RH ...................................................................... 83 Figure 26. Material kept at 89% RH and 30°C(Fungus Report) .......................... 84 Figure 27. (Side view) Comparison of Green Cell® foam kept at 25°C, 50%RH and 30°C, 89% RH ...................................................................... 84 Figure 28. (Front view) Comparison of Green Cell® foam kept at 25°C, 50%RH and 30°C, 96% RH ..................................................................... 85 Figure 29. Material kept at 96% RH and 30°C(Fungus Report) ........................ .85 Figure 30 (Side view) Comparison of Green Cell® foam kept at 25°C, 50%RH and 30°C, 96% RH ................................................................... 86 Figure 31. Comparison of samples maintained. at 84% RHI30°C and 50%RH /25°C. (Front view) ........................................................................ 88 Figure 32. Comparison of samples maintained at 84% RH/ 30°C and 50%RH /25°C (Side view) ........................................................................ 88 Figure 33. Comparison of samples maintained at 75% RH/ 30°C and 50%RH/25°C. (Side View) ........................................................................ 89 Figure 34. Comparison of samples maintained at 75% RH/ 30°C and 50%RH /25°C. (Front View) ........................................................................ 89 Figure 35. Net Change in thickness at 30°C at different humidity conditions ........... 90 Figure 36. Change in Width at 30°C at different humidity conditions ................... 91 Figure 37. Change of length at 30°C and different humidity conditions ................. 92 Figure No.38 (a and b). Comparison of samples kept at 95% RH, 30°C and 50%RH and 25°C. (Front View) ................................................................. 93 Figure 39. Comparison of 2-inch fresh and three month old material (side view) ...... 94 Figure 40. Comparison of l-inch fresh and three month old material ..................... 94 xii Figure 41. Figure 42. Figure 43. Figure 44. Figure 45. Figure 46. Figure 47. Figure 48. Figure 49. Figure 50. Figure 51. Figure 52. Figure 53. Figure 54. Figure 55. Figure 56. Figure 57. Figure 58. Figure 59. Figure 60. Graph between Time (days) Vs Thickness of Green Cell® foam at 25°C and 50%RH at constant load(* l-inch Green Cell® foam .......... 96 Graph between Time (days) Vs Thickness of Green Cell® foam at 25°C and 50%RH at constant load(* 2-inch Green Cell® foam) ......... 97 Change in thickness under load at 25°C and 50%RH for 1 inch and 2-inch GCF .................................................................................... 97 Relationship between change Thickness under constant load at 25°C and 50% RH(* 2-inch Green Cell® foam) ........................................... 99 Plot between the moisture content (%) and relative humidity RH (%). ....102 Plot between the moisture content (%) and relative humidity RH (%). ....103 Plot between the moisture content (%) and relative humidity RH (%). 104 Sorption isotherm of GCF at 20°C .............................................. 104 Sorption isotherm of GCF at 30°C .............................................. 104 Sorption isotherm of GCF at 25°C .............................................. 105 Plot of aw/Me and water activity at 20°C ....................................... 106 Comparison of Moisture sorption isotherm for Green Cell Foam based on experimental data and GAB model at 20°C .................................... 107 Graph between aw/Me and water activity at 20°C ............................ 108 Moisture sorption isotherm of Green Cell® foam at 25°C .................... 108 Graph between moisture equilibrium content vs. Water activity 30°C and different relative humidity conditions ............................ 109 Comparison of the moisture sorption isotherm (GAB and experimental) of Green Cell® Foam at 30°C ...................................................... 110 Fungus report at 20°C and 96% RH ............................................ 111 Comparison of fresh sample and material kept at RH75% and 30°C. . .. 112 Comparison of fresh sample and material kept at RH 95% and 30°C. .. 112 Net Change in weight at 30°C and different humidity conditions ........... 114 xiii Figure G1. Graph between G value and Time (days) ....................................... 132 Figure G 2. Graph between G values and Relative Humidity conditions (RH%) ....... 133 Figure G 3. Comparison of Green Cell® foam material kept at 50% RH, 25°C and 11% RH, 30°C. (Front view) .................................................... 137 Figure G 4. Comparison of Green Cell foam material kept at 50% RH, 25°C and 11% RH, 30°C. (Side view) ........................................................ 137 Figure G 5. Comparison of Green Cell® foam material kept at 50% RH , 25°C and 43% RH, 30°C.(Front view) ............................................... . 138 Figure G6. Comparison of Green Cell foam material kept at 50% RH, 25°C and 43% RH ,30°C.(Side view) .................................................. 138 Figure G 7. Comparison of Green Cell foam material kept at 50% RH, 25C and 43% RH ,30C.(Front view) ................................................ 139 Figure G 8. Comparison of Green Cell foam material kept at 50% RH, 25°C and 43% RH, 30°C.(Side view) ................................................ 139 Figure Dl-a. Dimensional changes at 11% RH and 30°C .................................... 141 Figure Dl-b.Weight changes at 11% RH and 30°C ........................................... 142 Figure D 2. Dimensional changes at 43% RH and 30°C ..................................... 147 Figure D 3. Moisture gain/loss at 43% RH and 30°C ........................................ 147 Figure D 4. Dimensional changes at 56% RH and 30°C .................................. 152 Figure D5. Moisture gain/loss at 56% RH and 30°C ......................................... 152 Figure D6. Dimensional changes at 75% RH and 30°C ..................................... 157 Figure D 7. Moisture gain/loss at 75% RH and 30°C ......................................... 158 Figure D 8. Dimensional changes at 84% RH and 30°C ..................................... 164 Figure D9. Moisture gain/loss 84% RH and 30°C ........................................... 164 Figure D10.Dimensional changes at 89% RH and 30°C .................................... 169 xiv Figure D 11.Moisture gain/loss at 89% RH and 30°C ........................................ 169 Figure D 12.Dimensional changes at 95% RH and 30°C .................................... 174 Figure D13. Moisture loss/gain at 95% RH and 30°C ........................................ 174 XV \\ \\ \\ \\ Nomenclature D: density M = mass of the specimen L1 = length of the specimen L2 = width of the specimen T = original thickness of the specimen in H = free fall drop height Vi = measured impact velocity G = acceleration due to gravity 386 Dynamic set can be calculated T = original thickness of the specimen F = thickness of specimen after test W, = Initial weigh of the product Wd = Final weigh of the product We: Equilibrium or final weight of the product Wiz Initial weight of the product Mi: Initial moisture content of the product Me: Equilibrium moisture content lb:pounds in: Inches in/sec: inches per second sec: second - xvi in Hg : inches of mercury psi : pounds per inches g: grams inches/sec2: acceleration lb/ft3: pounds per feet cube. pcf : pounds per feet cube BTU/lb: British thermal unit per pound Temp. : Temperature %RH : Percentage relative Humidity GCF : Green Cell® Foam Aw : Net weight AV : Change in velocity xvii IV Tl: NT Sl.’ \\ \ Ht bi FL) rt 0? \‘x INTRODUCTION Through plastic engineering, it was recognized that expanded structures foams could be easily achieved with polymers, especially in thermally reversible plastics. During the twentieth century, polymer synthesis was greatly enhanced to improve polymer structures. Several methods were developed to create a broad range of polymer structures during the middle and later part of this century. This was the era when industrial foams were developed. Also during this time, companies and municipalities faced major problems in disposing of plastic foams because they are lightweight and bulky and do not lend themselves to a viable economic and environmentally responsible recycling operation because they are expensive to handle and transport. Synthetic foams are not biodegradable, which makes disposal in soil or composting operations untenable. Further, issues such as sustainability, industrial ecology, biodegradability, and recyclability are becoming major considerations in a company’s product packaging design, especially with single use disposable packaging. There is thus, a market need for bio-based, biodegradable foam plastic packaging that can be safely and effectively disposed of in soil or in composting operations, and that has all . . ® . of the current foam plastics performance requrrements. Green Cell foam rs a commercially available, biodegradable foam produced from a proprietary cornstarch. It has recently become available in a variety of laminations and constructions. To compete with other presently available synthetic plastic foams, Green Cell® must have similar performance characteristics. Cushioning and thermal resistance (R-value) are 6V. SV‘ do 0? fundamental properties required for the foam to function act as a Packaging material for insulating and cushioning applications. Since Green Cell® is biodegradable, it will absorb some moisture, which will likely affect the above preperties. ASTM standard 1596 was used to determine cushioning characteristics at 25°C and 50%RH and these results were compared with the published data of other synthetic plastic foams available in the market. l-inch and. 2-inch thick Green Cell® foams were evaluated. Green Cell® foam having a 2-inch thickness had G values similar to other ® synthetic plastic foams. However, l-inch thick Green Cell foam had lower G values at lower static stress, but at higher static stress showed significantly higher G values as . . ® compared to the synthetic plastic foams. Green Cell foam was also stored at seven different relative humidity conditions at 30°C for two months and then tested to determine its G values. Another experiment was conducted to determine the time effect on G values and it was observed that G values decreased with passage of time. The density of 2-inch thick Green Cell® foam was determined to be 3.37lbs/ft3, while 1- inch thick foam had a density of 3.03Ibs/ft3. Change of thickness under load at standards conditions and at ambient conditions was also observed. No significant change in thickness was observed. Material behavior at ambient conditions was also observed. One inch and two inch thick material was kept under observation at ambient conditions for about three months where relative humidity and temperature varied between 50%-85% and 70°F-80°F. Significant increase in thickness was observed, demonstrating that the material is hygroscopic. 3 51 31% m3 N0 for is. It“ Cl C. Dimensional changes were observed at different humidity conditions and at 30 °C (86°F) after three weeks. The most expansion in dimensional characteristics occurred at 75% and 84% relative humidity and the material gained moisture at these conditions. The material also gained moisture, but shrunk at higher humidity conditions (88% and 95%). No significant dimensional change was observed at 11%, 43% and 54% RH. Moisture sorption isotherms at three temperatures (20°C, 25°Cand 30°C) were developed to determine its morsture sensrtrvrty. Initial morsture content of Green Cell Foam was found to be =0.1263 gHZO/g solid. GAB model was used to develop the sorption isotherms. GAB model results were compared with experimental values. The ice melt method was used to measure the package insulating ability and the thermal resistance (R- value). R-values of EPS and Green Cell® coolers were determined at standard conditions (50%RH, 72°F) and at 86°C, 80%RH. EPS has a 10% higher R-value than Green Cell® foam at standard conditions. But R-value of EPS cooler was found to be 20% higher at 86°F and 80%RH reflecting that Green Cell® foam degrades with increase rn temperature and relative humidity. Green Cell prcks up morsture, WhICh increased its thermal conductivity and lowered its R- Value. Biodegradable packaging materials will find niche markets, as long as their properties are comparable. To be used more broadly, Green Cell® foam, must be modified to both control its hygroscopic properties and weight problems (Green Cell® foam has high density). In the near future, the farm may make a significant contribution for non- traditional based uses of starch. 1.] IL“ fa 1'61 51" Gr 3? f") II- CHAPTER 1 LITERATURE REVIEW 1.1 Introduction The discovery of Bioplastic is presented in the feature article “How green are green Plastics” by Tillman U. Gemgross, and Steven C.Slater. The author starts the paragraph in the following way, “Driving down a dusty gravel road in central Iowa, a farmer gazes toward the horizon at rows of tall, leafy corn plants shuddering in the breeze as far as the eye can see. The farmer smiles to himself, because he knows something about his crop that few people realize. Not only are kernels of corn growing in the ears, but also granules of plastic are sprouting in stalks and leaves”[46]. Growing plastics, which seems achievable in the foreseeable future, looks more appealing than manufacturing plastic in petrochemical factories. According to the article ‘how green are green plastics’, “the plastic manufactured in the petrochemical factories consume about 270 million tons of oil and gas every year worldwide. Fossil fuel is the basic source, which provides both the power and the raw materials that transform crude oil into common plastic. It is difficult to imagine everyday life without plastic. But the sustainability of that production has increasingly been called into question. Known global reserves of oil are expected to run low in approximately 80 years, natural gas in 70 years and coal in 700 years but the economic impact of their depletion could bit much sooner. As the resources diminish, prices will go up—a reality that has not escaped the attention of policymakers”[46]. Biochemical engineers are pleased by the discovery of bioplastics/biodegradable plastics. Plant based plastic can be “Green” in two ways, plastic can be made from a renewable resource and it can break down upon disposal [16]. Using natural biopolymers is not totally a new idea. In one form or another, green plastics have been around for a long time. A brief review of green plastics (biodegradable plastics) is followed by a review of plastic foams. 1.2 History 1.21. Early History Some natural resin was used even during the early Roman and Middle Eastern times. Like amber and shellac, gutta (one of the series of small drop like ornaments on a Doric entablature.), percha‘s name has been mentioned throughout history. Native Americans used to make ladles and spoons from animal horns long before there was any European contact. In Europe, molded horn jewelry and snuflboxes were very popular in the eighteenth century [16]. 1.22. 1800’s Meaningful commercialization of bioplastics actually began during the middle of the nineteenth century. An American inventor, John Wesley Hyatt Jr. was looking for a substitute for ivory in the manufacture of billiard balls. He was able to patent a cellulose derivative for coating non-ivory billiard balls in 1869. His effort was, however, affected by the coating's flammability. Balls were occasionally ignited when lit cigars accidentally came into contact with them. Hyatt did not loose his focus and continued working on this pm: “it: 1.23 35 . 4‘? 1. er‘ \V.‘ CO: CT‘ project and soon developed celluloid, the first widely used plastic. Today it is most widely known for its use in photograph and movie films [16]. 1.23 1900’s In the 19005 the history of plastics changed dramatically, as petroleum started to emerge as a source of firel and of chemicals. Early bioplastics were replaced by plastics made from synthetic polymers. The production of plastics occurred on a very large scale after World War II, and continues to the present time [16]. 1.24 1920’s In the 19205 Henry Ford experimented using soybeans in the manufacture of automobiles. He had a desire to find non-food applications for agricultural surpluses, which existed as they do now. Soy plastics were used in number of automobile parts, like steering wheels, interior trim, and dashboard panels. Ford was able to produce a complete prototype "plastic car." He exhibited the prototype with great fanfare in 1941 but was not able to commercialize a new plastic car by the end of that year, because of a variety of reasons. At this point, World War II played a role; armament work supplanted almost everything else, and steel shortages limited all non-defense production. Today, plastic automobile parts are common, but the use of plastics made from renewable raw materials got side-tracked [16]. 1.25 1960’s Cellophane is a well-established bioplastic. This material is derived from cellulose. Its peak production was recorded during the 1960’s but it is still being used in packaging for candy, cigarettes, and other articles though its total usage in Packaging has substantially decreased [16]. 1.26 The 2000’s and Beyond Demand for plastics material is continually growing and it is not abating. The plastics industry is an important component of any country’s economy in today’s world. The US. plastics industry has over 20,000 facilities that produce or distribute materials or products. The industry also employs over 1.5 million workers, and ship over $300 billion in products each year [16]. The plastics industry does have some concerns, however pressures relating to waste and diminishing resources are major hurdles that are leading many to re-discover natural polymers and use them as materials for manufacturing and industry. Because of this, there is an increasing interest in a new generation of green /biodegradable plastics [16]. Research on starch-based products has taken place in many countries around the world. The Australian Government funded in 1995 a research project to develop starch-based plastics from corn and wheat, using water and glycerin as a plasticizer. The biodegradable plastic society was formed in 1989 with 48 member companies located mainly in Japan. By 1990, the membership increased to 69 companies, including a significant number of non-Japanese members. In 1992 a US Bio/environmental society was formed and had over 200 members by 1998. As an example, many companies sell Oi fl I '.1 starch based foam peanuts for loose fill packaging as a substitute for expanded polystyrene [21]. 1.3 History of Plastic Foam The texture of matter has been modified since ancient times. Survival of the human race depended on softening rice and other foods using yeast, water and heat to make these ingredients soft enough so that they would be acceptable to digestive organs. These techniques were designed to create expanded structures. These structure can be found everywhere in nature, ranging from tree pulp to marine organisms [46]. Through plastics engineering, it was recognized that expanded structures could be easily achieved in polymers, especially in thermally reversible plastics. During the twentieth century, polymer synthesis was upgraded to enhance the polymer structure. Several methods were developed to create a broad range of polymeric products, during the middle of this century. This is the era when industrial foams were developed. [46] 1.31 Early History (2680-2565 B.C) It may have stated before 2680 BC, no one knows for sure, but the architects of Stonehenge engaged the services and discoveries of foam masons. [7] Figure 1. Historic pyramids (2680-2565 B.C) Phg. his {55’ 311'. Pharoah Rameses II (2680-2565 B.C) presented the idea of a gigantic stone pyramid to his engineers. They were, at that time hardly enthusiastic. No one wanted to spend the rest of his career—watching slaves, stacking stones on top of each other. Yunghotstuff II , an intelligent bright engineer presented the idea of using foam for the pyramids. He explained that the lightweight blocks would skim easily over the sand, and would be easily elevated, as it grew taller. This also resulted in the tremendous reduction in building cost. After that, pyramids popped up all over Egypt and they remain there resisting the elements of sun and sand, a memorial to human ingenuity and the power of foam [7]. 1.32 1000-1500 History Recent ethnographic studies of today’s Easter Islanders have revealed a fondness for decorating the front’s parts of their homes with small icons. Experts have concluded that they were simply large-scale foam lawn ornaments. The ancient figures on Easter Island are a confirmation of the durability of well-build foam art [7]. Ea t r tiara... Figure 2. Easter island (1000-1500) 1.33 1887 History When French Sculptor Fredeic Auguste Bartholdi was commissioned to build a monumental statue, arcane zoning regulations could have blocked the famous statue installation. Stat e of rty Figure 3. Statue of Liberty (1887) Before the American Revolution, New York City ordinance 56-0894 required that all structures and vessels in New York Harbor be able to float. Originally the Statue of Liberty had been originally commissioned to be built of bronze, sculptor Bartholdi realized that his project could be easily scuttled if he could not propose an alternative construction material. Bartholdi’s own countryman Gustave Eiffel was studying the use of foam as substitute for steel in large engineering constructions. Eiffel was persuaded to share his patented procedure with the sculptor. The bottom line is that, “it was foam, francs and delightful Bordeaux that saved the jour” [7]. Polymer synthesis and processing have been improved since the middle of the twentieth century. Many foaming methods have been started and transferred from lab scale to industrial scale [22]. 1.4 Biodegradability: “The term biodegradability means that living organisms can use the plastic as a food source, transforming its chemical structure within a reasonable period of time” [5]. In practice we rely on microorganisms to transform carbon in the polymer to C02, CH4 and other small molecules. Usually the time period required is several weeks to months. One way to obtain biodegradable plastic is to use natural polymers, that is, those formed by living organisms [14]. In figure 4, the basic “Central Principle” for biodegradation of polymers is shown in the form of a schematic diagram. Polymer l (1 Conjugation, oxidation or hydrolysis Outside Cell Polymerization l (Exo or Endo enzymes) Depolymerization 1 Mineralization I. inside the Cell /\ H20 C02 _. v Biomass Figure 4. Schematic diagram for biodegradation of polymers ll This process consists of two key steps: first, depolymerization or chain cleavage and second, mineralization. [14] The first step normally occurs outside of the organism (usually bacteria or fungi due to the size of the polymer chain and insoluble nature of many of the polymers). In this step, extra cellular enzymes are responsible for acting either endo (random cleavage of the internal linkage of the polymer main chains) or exo (sequential cleavage of the terminal monomer units in the main chain). [14] Sufficiently small oligomeric chains are formed and then transported into the cell where they are mineralized. The cell usually derives metabolic energy from the mineralization process and the products, apart from ATP, are gases (e.g. C02, CH4, N2), water salts, minerals and biomass [14]. Traditional plastics cannot undergo biodegradation; the reason is because of their long polymer chains. These long chain polymers are too large and too tightly bonded such that they are very difficult to break apart, and thus can not be transformed into relatively simple components [16]. However, plastics based on natural plant polymers, such as wheat or cornstarch have molecules that are readily attacked and broken down by microbes [16]. 1.41 Key Elements in Biodegradation There are three key elements in the biodegradation process as shown in the following diagram. If any of the elements (below) is lacking, then the entire process will stop. 12 Biodegradation Substrate Organisms 1) Chemical bond Environment 1) Appropriate enzymes 2) Branching 1) Temperature 2) Appropriate enzymes 3) Hydrophilicity/ 2) Oxygen Level Hydrophobicity 3) Moisture 3) Co- metabolism 4) Stereochemistry 4) Salts 4) Aerobic,anaerobic,facultative 5) Molecular weight 5) Metals 5) Enzymes kinetics 6) Chain flexibility 6) Trace nutrients 6) Inhibitors/inducers 7) Crytalinity 7) PH 7) Enzyme location 8) Interation with co 8) Redox potential (intra,extra-cellular) polymer coatings 9) Stability 8) Predators 9) Surface area 10) Pressur 11) Alternate carbon 12) Light Figure 5. Key elements in the biodegradation process [14] 13 1.42 Bioplastics: Bioplastics are materials with plastic-like properties made from renewable resources such as corn, wheat, rice, soy and potato: Biopolymer(s) + Plasticizer(s) + other additive(s) = Bioplastic. Biopolymers are inherently biodegradable. Biopolymers almost always have oxygen or nitrogen atoms in their polymer backbones. This particular feature is mainly responsible for their biodegradability [16]. There are three main new and important types of bio plastics material (carbohydrates, Lignins and Polyesters). They differ according to the means of commercially producing the resins from which the bioplastics are produced. There are also ready-made polymers existing in nature, which can be used in manufacturing bioplastics. Starch being the prime example [16]. Figure 6 shows the basic structure of a Starch Molecule. [49] 14 1.42.1 Starch Structure of Stargh Polymers CHZOH CHZOH H H OH H OH H _—o __ H H H H Linesr a —l-4- glucan—amylose 200 to 2000 anhydroglucose units 6) H H HZOH HO EH2 CHZOH Branched polymer —amylopectin a -1,4-glucan with 1,6-glycosidic linked braches containing 20-30 anhydroglucose units Figure no. 6 The basic structure of a Starch Molecule Starch is the main component of most human and animal diets. It is found in the storage organs of plants in the form of partially crystalline water-insoluble granules. [49] Starch is composed of anhydroglucose units, which are the major source of storage energy in various plants in nature. It can be widely found in cereal grain seeds (e.g. corn, wheat, rice, sorghum), tubers (e.g. potatoes), roots (cassava, sweet potatoes, arrowroot), legume seeds (e.g. peas beans and lentils), fruits and leaves (tobacco). [47] The starch molecule consists of two master polymer components, amylose and amylopectin. Their structure and the relative amount of both populations play an important role in the starch properties. The amylose content and degree of polymerization 15 (DP) are important in the physical, chemical and technological properties of starch. [46]. Cornstarch typically consists of 28% amylase and 72 % amyl pectin but it can be genetically modified to have as much as 85%. [22] Starch based material is important not only because it is the least expensive material but also it can be made into a thermoplastic when properly plasticised with water or other plasticizers. Therefore, starch formulations can be made into film or container by any method used for synthetic resins like extrusion, injection molding and thermo- forming [16]. The main limitations of starch-based formulations are physical/chemical properties such as poor water resistance and modest strength [16]. Starch based materials are being used for a number of applications and several major companies produce starch based resins. These resins further have been used to manufacture agriculture covers, compost bags and trash bin liners, house hold items such as disposable bowls, eating utensils and straws, single use disposable packaging film, diaper backing, disposable golf tees and personal hygiene articles like combs and disposable razors. [16] 1.43 Retrogradation The aging of starch systems has a major effect on the quality of many products. Starch- based foods, such as bread and dough, stale with the passage of time. Low fat baked, or convenience foods are particularly susceptible. Furthermore in non-food uses of starches, for example in paper and adhesives applications, retrogradation affects the processing and final properties of the product. Similarly, one of the most important practical problems with recently developed starch plastics is their tendency to become brittle over time, a 16 process analogous to the staling process in baked goods. [47] The basic definition of retrogradation is the returning to a former state or passing from a more complex to a simpler biological form. [30] 1.43.1 Retrogradation process of Starch When Starch is heated with water, it gelatinizes and the amylopectin is swelled. Starch particles then proceed to harden. This process is called retrogradation. [39] F. Lionetto et all, in his paper [24] described the process of retrogradation. Starch consists of mainly two polysaccharides, amylose (linear polymer) and amylopectin (highly branched macromolecule). Amylopectin is believed to be the main contributor to the crystallinity of the starch granule [24]. The starch granules are made of concentric amorphous and semi-crystalline growth rings. Starch granules are insoluble in cold water, but, when heated in the presence of excess water, they swell. This swelling is reversible up to a certain temperature. This particular temperature is known as the gelatinsation temperature, where a more pronounced swelling takes place, accompanying the melting of the crystalline regions. Principally linear amylose becomes soluble and leaches out of the disrupted granule. In addition to thermal processing, the conversion of starch from its native partially crystalline granular structure to a polymeric solution/melt and subsequent molecular degradation can be driven by mechanical shear (e. g. in extrusion), chemical (e. g. through the use of solvents) and biochemical (e.g. through enzymatic hydrolysis) processes, etc [24]. Upon cooling, and the during early storage stage, amylose gelation or retrogradation occurs while in longer term storage (hours-weeks depending on composition and storage 17 conditions), amylopectin retrogradation occurs, which leads to the partial recrystallisation of amylopectin producing an increase of firmness and a decrease of water-holding capacity [24]. Retrogradation occurs because gelatinized starch is often super cooled and stored below its melting temperature and therefore is not in thermodynamic equilibrium. Molecular packing and crystallization occurs during storage. Starch retrogradation is scientifically and technologically important since it leads to significant changes in the mechanical properties of starch-based products and thus greatly affects their sensory (e.g. texture and flavor perception), nutritional (availability) and processing (shredding, cutting, etc.) characteristics. [24] This is further described by Zhenghoug Chen [50] in his dissertation; starch pastes may become cloudy and eventually deposit an insoluble white precipitate during storage. This phenomenon is caused by recystallization of starch molecules. Amylose is considered primarily responsible for the short —term retrogradation process due to the fact that the dissolved amylose molecules reorient in parallel alignment. But the long-term retrogadation is represented by slow recrystallization of the outer branches of amylopectin [50]. Basically the rate and the extent of retrogradation increase with an increasing amount of amylose. Retrogradation also depends on starch concentration, storage temperature, PH, process temperature, and the composition of the starch paste. Retrogradation is generally stimulated by high starch concentration, low storage temperature and PH values between 5-7. [50] 18 1.44 Thermal Insulation Defining R-Value The demand for quality building insulation has soared during the 1970’s. At that time many new products were introduced with many conflicting claims pertaining to their insulating abilities. The federal Trade Commission with the participation and support of the insulation industry created an objective method to report the performance of residential insulating materials. This method was called the R-value Rule. [23] Plastic foams are becoming more and more important in insulation. Price, performance and special design considerations are the most significant features, to consider in selecting any foam to be used for insulation. [12] To reduce winter heat loss and summer heat gain, plastic foam is being more prominent than other materials because of their significant energy saving capability. Plastic foam insulation is the only viable method for building foundation walls and flat, steel deck roofs, and for packaging needs [23] Other insulating materials like mineral wood and fiberglass are being used in the building industry as alternatives to foam board stock. Vacuum panels are also being used for building insulation applications. Insulation for flat roofs and below grade foundation walls requires compressive strength and the moisture resistance of closed cell foam. This cannot be found with other insulating materials. [12] The R- value gives information regarding product labeling (R-value) and advertising, and mandates specific ASTM methods for thermal testing. The basic purpose of the R-value Rule is to create a level —playing field for competing insulating materials. 19 “The R-value Rule has been helpful in comparing different brands of the same type of insulating materials,” said Betsy de Campos, executive director of EPSMA, “ but as more sophisticated materials and higher technology construction systems are introduced into the building industry we find that the R- value of the material does not tell the whole story.”[23] R- value is based on the mathematical term known as R- factor. The term R- value was developed to represent the ability of an insulation material to restrict flow. Thermal resistance® of a material is its resistance to heat flow and is expressed as the reciprocal of the material thermal conductivity. Simply put, the greater the R-Value the better the insulation. [23] 1.45 Green Cell® Foam Extruded starch foam is used as a loose fill packaging material (pallets or peanuts). Green Cell® foam is a commercially available, biodegradable foam material produced from a proprietary cornstarch. It has recently become available in a variety of laminations and constructions. Green Cell foam can be used as a cushioning material and in applications where thermal insulation is essential [5]. KTM Industries, Inc. develops, manufactures and markets new bioplastic technologies for applications that incorporate proprietary, non-toxic, environmentally safe bio plastics like Green Cell® Foam. Large-scale production of these polymers is being developed because they have been found to have important commercial uses [5]. Typical current applications for the use of Green Cell® Foam can be seen in Figures 7 to 10. 20 "1. : (1":1' Fig " .11.! . ‘5 _Is .. -.- ‘I- & fly» .. r .- m '9'! I . Figure 7. Die Cut Figures 7 and 8. Figure 9. Medical Shipper Figure 10. Shipping Coolers Figure 8. Die Cut Laminated End Cap Green Cell® Foam is presently used as a Die Cut and as a Die Cut Laminated End Cap Figure 9 and 10. The major uses of Green Cell® Foam are for Medical Shipper and for shipping Coolers purposes. [5] 21 I’) ""3 1.45.1 Composition of Green Cell® Foam. 1) Green Cell foam is made from Starch, HYLON VII (High Amylose, 70% Amylose) with an inherent moisture content of 1’ 1.2%. 2) Water used as the plasticizing agent, as well as the Blowing agent (IO-12% of the dry feed) for all products. 3) BLOX (Dupont), to provide adhesion and durability resin with the flexibility and process ability of thermoplastic resins. Green Cell® foam is made in thick nesses (t) of 1 and 2-inches. [5] 1.46 Foam Definition According to S.T.Lee author of the foam extrusion book, “Foam can be defined as a gaseous void surrounded by a much denser continuum matrix, which is usually in a liquid or solid phase”. This phenomenon widely exists in nature, in cellulose wood, and marine organisms. Foams can also be made using different synthesis processes (foamed plastics). [45] Plastics foams can be classified in different ways, for instance, as flexible and rigid, as sheet or board, as low-density or high-density, as closed cell and open cell, and by cell size as foam and micro cellular. To minimize confusion, it is desirable to have a standard nomenclature for foam such as the one from IUPAC. In 1996, over six billion pounds (three metric tons) of synthetic foamed plastics were consumed in the United States. Today’s, this material is widely used for a variety of packaging applications. [45] 22 IiIA 1.47 Types of commercial foams Types of commercial foams are shown in the table No.1 and Major types of foam and their applications can also be seen in figure 11,. Table No.1. Major types of commercial plastic foam Types of Foam Types of Foams Poly styrene foam Pyranyl foam Poly Urethane foam Miscellaneous cellular plastics foams Poly olefin foam Synthetic rubber and silicon foam Polyvinyl-chloride foam Inorganic foams Phenolic foam Expanded beads and spheres Urea-formaldehyde foam Acrylonitrile and acrylate copolymer foams Epoxy foam 23 Poly etymno PIR I] '- 60-an *— Rigid Pom-1e lneulation —" — Phenolc < 5% ——I: b Appll-noo -— Rigid Pom -I: Id PD — .. m... ___r: :~,.,,,,,,M,,“__ Polyetymne- —'E M % Polyolefln ———-C Packaging m neulatlon __ Polyurelhene Moulded —-—- Polyolofln Board about ---—- Polyolefln __.__._._ Flexible Cushioning ‘ "9““ Polyurethane Moulded '———— Polyolefln m Integral Sldn Polyurethane -—-—— 83W Sheet Poly-olefin —— Polyolefin —— E a.“ —-——E _ Polystyrene Figure 11. Major types of foam materials and their applications Boerdmck PIpO Boom flock/F ioxblo Faced Laminated Roofing Sandwich Panel. 0 SproyIPour-in-Plaoo Rooting Slabaaook Plpe-In-Plpo Boerdelock Pipe HVAC Roll-lg embrafireezete Picnic BoxedOther Sandwich Penele Sandwich Panels Single Service Ueee Food Packaging Mlec. Packaging Frmiture Cushion Pad-raging Cushion Packaging Cuehlon Packaging Automotive Interior: Corp“ Underley Funlture Sodding Funltun Automotive Cushioning Auto Banner Systema Auto Bumper SW Steering WM. Flotation - Life Vests Flotation Flotation A more description of these foams and these uses in packaging follows. 24 1.47.1 Polystyrene foam Modern man has known about styrene for centuries. Styrene is present as a naturally occurring substance in many foods and beverages including wheat, beef, strawberries, peanuts and coffee beans. It is also found in the spice cinnamon. Its chemical structure is similar to cinnamic aldehyde (the chemical component that elicits cinnamon's flavor). Polystyrene foam is one of the rigid foams currently sold, and in fact dominates the market with urethane foam second. [13] Polystyrene foam was made first in Great Britain in 1943 but the early development was accomplished in Sweden during the mid 1930’s. DOW Chemicals Company was first introduced as extruded polystyrene foam in the United States in 1943.The foam was used during world war II for construction of life rafts on troops transports and for floating equipment to shore. [l 3] Styrene is a primary raw material and is a petroleum by-product. Styrene played a vital role during World War II. It was also used in the production of synthetic rubber during that time. After the war, the styrene utilization shifted towards the manufacturing of commercial polystyrene products. Synthetic styrene is also used in the manufacture of products such as automobile parts, electronic components, boats, recreational vehicles, and synthetic rubbers. [37] Polystyrene (PS) meets tight (stringent) US. FDA standards for use in food contact packaging and is safe for consumers. Health organizations encourage the use of single- use food service products, including polystyrene, because they provide increased food safety. [37] 25 All packaging (glass, aluminum, paper, and plastic - including polystyrene) contain substances, which can "migrate," or transfer, to foods or beverages. The FDA (Food and Drug Administration) monitors and regulates residual levels of different components in food packaging to ensure safe packaging. [37] Rigid thermoplastic polystyrene foam is available in densities ranging from 1pcf to over 20 pcf. PS foam can be purchased as a film, sheet and rod or as large slabs and containers made by steam molding techniques. Foamed film and sheet can be thermoformed into different low cost trays and for other uses in the packaging industry. The thermal insulation properties and low cost of polystyrene foam make it competitive with other commercial insulating materials. Because of its closed cell structure, PS foam has excellent water resistance and low water vapor transmission. These properties make it possible to use as a support for floating docks and for other floatation applications. The closed cell structure and inert surface render polystyrene foams resistant to rot and mold growth. [13] Manufacturing of poly styrene foam Polystyrene foam can be produced either by direct extrusion and expansion of foamable beads and granules or by the injection of a blowing agent into the resin at high pressure, followed by expansion at atmospheric pressure. [13] The two basic methods of manufacturing are being discussed below. 1) Dow Chemical Process: In this method, polystyrene and expanding agent, usually a low —boiling chlorocarbon such as methyl chloride, are blended together and extruded. [13] 26 hr] I'll r" 2) Badisch Anilin and Soda Fabrik process: In this method the styrene monomer and a low boiling hydrocarbon are polymerized together. The product is ground into chips and ultimately converted into low-density foam by extrusion. [13] The production of polystyrene foam from expandable beads is as follows; a) Preparation of expandable beads and pellets. b) Pre expansion of beads. c) Conditioning of the expanded beads. d) Molding of the expanded beads. e) Extrusion of expandable bead and pellets to form sheet and film. The most important and the major step in producing foam sheet is Extrusion. Three major systems are used to produce polystyrene foam sheet and film for various applications. Two systems involve the extrusion of expandable high molecular weight polystyrene beads or pellets containing pentane as a blowing agent (6-7%) to produce a thin, low- density sheet and film. Pellets are being used more as a preferred feedstock than foamable beads because they give a more uniform feed. [13] The third system incorporates two stages (bead preparation and extrusion expansion) into one step. In the one step system, high molecular weight crystals of polystyrene are used as a feedstock and produce foam sheet by addition of hydrocarbon or methyl chloride as a blowing agent during the extrusion process. This system produces a low-density sheet and / or film and is considered to have many economic advantages over the two-stage extrusion of expandable beads or pellets. [13] Polyurethane foam has one major advantage over PS and that is that it can be “put in place” or “on the site placement”. High temperature is a requirement in the 27 r; ’I manufacturing of polystyrene foam, thus on the site foaming is not feasible. PS beads require a large quantity of heat to induce foaming, therefore, in place foaming is not possible. However, the low cost of PS foams (6-8c/bd ft) is a strong incentive for its use. [13] Environmental concerns and blowing agents Polystyrene foam products are 95 percent air and only five percent polystyrene. When polystyrene foam packaging is produced, a blowing agent is used in the process. Most polystyrene foam products were never made using chlorofluorocarbons (CFCs) as a blowing agent. The very few polystyrene products that were made with CF Cs contained a very small portion of the nation's CFC use. According to the US. Environmental Protection Agency (EPA), only two to three percent of CFCs used in the United States in the 19805 went toward production of polystyrene packaging products. Polystyrene manufacturers exceeded government goals and timetables during the CFCs phase out period of in the late 19805. Polystyrene foam products are now manufactured using primarily two types of blowing agents: Pentane and Carbon Dioxide. [37] Pentane gas has no effect on the upper ozone layer, although, if not recovered, it can contribute to low-level smog formation. Therefore, manufacturers use state-of-the-art technology to capture pentane emissions. [37] Some manufacturers use carbon dioxide (CO; or other hydrocarbons in some cases) as an expansion agent for polystyrene foam. C02 is a non-toxic, non-flammable gas. It does not contribute to low-level smog, and has no stratospheric ozone depletion potential. In addition, the carbon dioxide used for this technology is recovered from existing 28 00111111 increi commercial and natural sources. As a result, the use of this blowing agent does not increase the levels of C02 in the atmosphere. [35] However, there is still serious concern regarding the use of polystyrene products as a food packaging material. Due to present economic conditions, polystyrene food service packaging is generally not recycled. Polystyrene protective packaging and the packaging non-durables (i.e., video/audio cassettes, agriculture trays, etc.) are the primary forms of polystyrene collected for recycling. The amount of polystyrene food service packaging that is recycled has decreased during this period. Non-food service packaging is not contaminated with food and other wastes, as is food service polystyrene packaging. Therefore, it is more cost-effective to recycle. Presently, food service polystyrene packaging is not recycled because it is not economically sustainable. It is important to note that because of unfavorable economics, no other post-consumer foodservice disposable material, including paper and paperboard, is recycled in a measurable way [28]. Properties Extruded polystyrene foam has been produced in densities ranging from 2.0pcf to 6.0pcf in many configurations. The properties and the quality of foam sheet depend on extrusion, pressure temperature, nucleating agent, polymer structure and other process variables. Low densities polystyrene foam is flexible and can be laminated to paper and high impact styrene sheet. [11]. Polystyrene foam is soluble in many organic solvents. Polystyrene foam is water repellent because of its aromatic structure and is unaffected by changes in RH. [28]. Figure 12 shows the basic structure of the polystyrene molecule. 29 Structure of Polystyrene Figure 12. The basic structure of polystyrene Since polystyrene foam is a thermoplastic, it has a well-defined softening point. The softening point of the foam is similar to that of the parent polymer and is independent of the volume fraction of gas present (density). The specific heat of the polymer depends on its structure. The specific heat of the cellular composite depends on both density and structure. The thermal expansion of the polystyrene foam mainly depends on polymer structure and is independent of density but affected by the closed cell structure. As polystyrene foam is an organic material, it can burn and since it is a thermoplastic it can melt. [12] The molecular weight (molecular size) of polystyrene determines the structure of both extruded polystyrene foam and styrene foam beads. Decreasing the molecular weight of polystyrene increases its sensitivity to shrinkage. In general, the following rules apply regarding the molecular weight of the polymer. 1) Cell size decreases as the molecular weight of the resin increases. 2) The boundary between expanded beads (where the beads are firsed to beads) is thicker for high molecular resins. [12] 30 J 1.47.2 Polyurethane Foam The manufacturing of flexible polyurethane foams is a large business. Polyurethane foams play a vital role in every day life. The foam is used in houses, cars, schools, work places, airlines and for packaging applications. [31] History Mankind’s curiosity, imagination and needs have pushed research and development to create a vast number of products. Once a basic product has been ‘invented’, then questions about its applications, uses and economical factors are considered.[38] Polyurethane was invented by Otto Bayer in the late 1930’s. Early in the 1940’s, some prestigious companies such as I.G. F arben of Germany, ICI of the United Kingdom and El. Dupont of the United States developed urethane systems for such applications as coatings for the Barrage balloon, synthetic bristles and submarine insulation/flotation. [38] Further development brought in new urethane products. These products greatly expanded the markets for flexible, rigid and energy-absorbing foams. This research led first to Poleset, then to Freon-free Poly-Set, and now our latest backfill system, Poly- Ground. [38] Forward Enterprises was a pioneer in the use of a rigid polyurethane foam to set direct- embedment utility structures. Numerous companies have investigated the effectiveness of the use of foam in areas of corrosion-protection and structural integrity for direct- embedment structures. [3 8] The long-term effectiveness of polyurethane foams has been established by Forward Enterprises and by E. I. Dupont. Their research showed that partial embedment of foam- 31 faced panels in soil for ten years “showed negligible deterioration of the foam and of the attached metal protected by the foam.”[3 8] Bayer has a vast variety of case studies of urethane foam applications for protecting metal structures from chemical attack, both above and below ground level. These show that urethane applications counteract the porosity of masonry structures. [3 8] Manufacturing process; The Urethane foam manufacturing process involves a series of complex chemical reactions. These reactions lead to the formation of many chemical bonds in addition to the urethane groups. The two most important reactions in the manufacturing of flexible urethane foam are the reaction between isocyanate and hydroxyl compounds (polyesters or polyester polyols) and the reaction between isocyanate and water. The former reaction is considered as the chain ——propagating reaction and is shown below. [13] O l | R—N=C=O+R‘ -—OH—> R _ NH—C_ o_R/ (Urathane) This reaction is common to both flexible and rigid polyurethane foam formation. [13] An alcohol molecule first reacts with an isocyanate to form an active complex. This complex firrther reacts with another alcohol, forming an interrnediately, which decomposes to produce the urethane group and free alcohol. The general expression for this type reaction may be written as follows: 32 R\NCO + catalyst —"—’ complex —* active hydrogen —’ Compounds ———> products + catalysts The second reaction is called the water —isocyanate reaction. This reaction is responsible for foam formation and liberation of carbon dioxide. The first step is the formation of unstable carbamic acid, which decomposes to form an amine and carbon dioxide. The thermal conductivity of the encapsulated gas is very important in insulation and because of that the second step is minimized in the production of closed cell rigid urethane foam. The blowing agent Freon is used in the later case, and the expansion of the foam is the result of the volatilization of the fluorocarbon, caused by the exothermic isocyanate alcohol reaction which is shown below. [13] O R—N=C=O+HZO ’[R NH_C_OH] ’ Carbamic acid R— NH2 + C02 The reaction mechanism is too slow to produce economical, commercial urethane foams. Catalysts are used to increase the reaction rate and to establish the proper balance between chain extension and the foaming reaction. It is essential to entrap the gas (CO2) efficiently and'to provide sufficient strength in the cell walls and struts at the end of the 33 TOP." 013? Ia. .; 1 St. 531C] hit C]? r‘.- rb v. foaming reaction to maintain the structure without collapse. For rigid insulation foams, a proper balance between exothermic chain —propagating reactions and endothermic volatilization of the Freon blowing agents is essential. The objective is to produce a stable foam during final curing of the structure. [13] A second important function of the catalysts in the foam reaction is to complete the reactions, resulting in a proper cure of the foam. Catalyst selection and concentration is governed by the type of foam to be made, the nature of the foaming process and the foam processing equipment and conditions available. [12] The most commonly employed catalysts are tertiary amines and organmetallic catalysts. [12] Types of polyurethane Foams: Currently urethane foam is primarily available by three types. 1) Flexible foams: These foams are based on a propylene oxide adduct of glycerol (3000 mol.wt.). The desired properties of the resulting foam are low density, high load bearing ability and low set. 2) Rigid Foams: These are made by both prepolymer and one shot processes. The one-shot method produces low cost, high performance foams. 3) Semi rigid Foams; Semi rigid foams are mainly used in the automotive industry where shock absorbing and elasticity are desired. [12] 34 Manufacturing Methods Foam properties are generally dependent upon the mode of preparation and the mechanical processes used. In general, three methods are used: 1. Poured in place, this method is used for filling irregular voids with foam. 2. Slab stock; this method is used in applications where foam can be most economically cut to required shape. 3. Sprayed; used in applications where field moldability is required. [13] Foam properties vary depending on how the foam is produced [13] Flexible foam Polyether polyols based on alkylene oxide adducts of simple polyhydric alcohols, highly active tin catalysts and alkyl silicon —polyoxyalkylene copolymer surfactants are the major components of one- shot urethane foam systems. These materials and other formulation components, together with processing variables, play a significant role in the successful production of foam. [13] In the one-shot system, a polyol and a diisocyanate, water, catalysts and other processing materials are mixed. Chain extension, cross-linking and foaming reactions take places within seconds during the gas foaming step. As the molecules line up and form a network, viscosity increases, the carbon dioxide released is retained in the bubble and within a few minutes the foam has turned into a solid cellular mass. [13] The major properties of flexible foam that influence its use are [32] 35 1. Density 2. Compression 3. Sag Factor 4. Fatigue loss 5. Hysteresis 6. Tensile 7. Elongation 8. Tear Density levels started out at around 2.0 lbs/cu. ft. The density levels were lowered as the industry became more competitive. Currently, the most popular foam has a density of 1.2-lbs/cu. ft, though there is a trend to increase densities up to 3.5—lbs./cu. ft. In most cases, except for high quality, high price items, it is best to maintain a minimum of 1.4- lbs./cu. ft. density. [32] Compression refers to a definition adopted by the American Society of Testing Materials (ASTM). By definition therefore, compression is "the load bearing capacity of a standard specimen indented by a circular compressor foot of 50 sq.in. at 25% deflection." The normally accepted standard is a piece of foam measuring 25 in. x 15 in. x 4 in. thick. Increasing the water in the formula and decreasing the amount of auxiliary blowing agent can increase compression during the production process. [32] Sag Factor is the compression of a piece of foam at 65% deflection divided by the compression at 25% deflection and expressed as a pure numeric. The higher the density, the higher the sag factor, regardless of the type of foam. The higher the sag factor, the 36 -l is” better the foam. The sag factor range on most foam is from a low of 2.0 to a high of 3.0. Any foam having a sag factor less than 2.0 is usually poor quality foam, which indicates that it was poorly manufactured. [32] Fatigue loss is a factor that describes what will happen to a cushion during service. Typically it predicts what the height loss and compression loss will be after it has been in service for some time. Inexpensive 1.32-lb./cu. Ft foam will have a height loss usually over 2 1/2 % with a compression loss of about 30%, whereas a 2.0 lb. urethane density foam will have height losses as low as 1/2% and compression losses as low as 10%. [32] Hysteresis loss is relative to compression readings. The lower the hysteresis loss (higher the resilience) the better the foam quality. No foam should have a hysteresis loss greater than 40%. If it does, generally there is something wrong with the foam. [32] Tensile, Elongation and tear are three material tests used to determine foam quality and are simple to perform. Tensile strength is the force required to pull apart a piece of foam and is expressed in pounds per square inch. Elongation is the amount the of foam will stretch before it pulls apart. Tear strength is the force required to actually tear the foam. The value is expressed in pounds per linear inch. [32] Rigid foam Rigid polyurethane foam has versatility in both directions because of its physical strength and mechanical properties. These qualities enable it to be used in a wide variety of multi- functional building products, which combine insulation with load bearing, sealing, impact resistance, weight and space saving, and ease of maintenance. [13] Rigid polyurethane 37 foam provides a high level of compression and shear strength, which is further enhanced by bonding with facing materials such as metal or plasterboard. [48] Low thermal conductivity Rigid polyurethane foam has one of the lowest thermal conductivity ratings of any insulant, which allows efficient retention of heat or, alternatively, maintenance of a refiigerated or frozen environment. [48] Effective insulation in all types of buildings is important in the conservation of non-renewable fossil fuels. [48] Adhesion The adhesion strength of polyurethane foam is extremely high. This strength develops during the short period between mixing and the final curing process. Due to its high adhesive strength, rigid polyurethane foam can be effectively bonded to a wide range of building facings. The adhesion is so strong that the bond strength is usually higher than the tensile or shear strength of the foam. [48] Compatibility/Stability Rigid polyurethane foam is compatible with a large number of building and packaging facings, including paper, foil, glass fiber, aluminum, plasterboard, plywood and bitumen. These materials add to the inherent strength of the foam, which enable its use as semi- structural panels and cladding and allowing foam to accept a variety of finishes so that it can operate effectively as a moisture barrier in conditions of high humidity. The water vapor permeability of rigid polyurethane foam is low and is enhanced in most building applications by the incorporation of a moisture barrier of polyethylene film or aluminum foil. [48] Rigid polyurethane foam provides excellent resistance to a wide range of chemicals, solvents and oils. [32] 38 Heat and Fire properties Like all organic building materials - wood, paper, plastics, paints - rigid polyurethane foam is combustible, although its ignitability and rate of burning can be modified to suit a variety of building applications and it can be formulated to meet the relevant national regulations. [48] Rigid polyurethane foam can be used in applications which experience exceptional extremes of temperature, from -200°C to +100°C. Density At low densities (e.g. 30kg/m3), the volume of polyurethane polymer in rigid polyurethane foam is around 3 per cent. The remaining 97 per cent of the foam is gas trapped within the cells, which provides the low themial conductivity properties. The lightness of the foam is an important aspect in terms of transportation, handling and ease of installation. [48] 1.47.3 Polyolefin foam Polymer Foams are used in many different types of applications and it is hard to find an area where they are not utilized. [28] Polyolefin Foams are a relatively recent development compared to the other types of foam. “Olefins” or “alkenes” are defined as unsaturated aliphatic hydrocarbons. Ethylene and propylene are the main monomers used for polyolefin foams, but dienes such as polyisoprene are also be included. The copolymers of ethylene and propylene (PP) are included, but not polyvinyl chloride (PVC), which is usually treated as a separate polymer class. The majority of these foams have densities <100 kilograms per cubic meter, and their microstructure consists of closed, polygonal cells with thin faces...” [32] 39 r—1 ‘7) '"1 \l The tremendous growth of polyolefin resins is well known to the plastic technologist or anyone else connected with the plastic industry. From its beginning in Europe in the early 1940’s, the production of low density polyethylene has risen to phenomenal heights (over 3.7 billion pounds in 19670.1n the early 1950’s plastic foams based on polyolefin resins first appeared commercially. Since then the market has increased, but not at the phenomenal rate of growth that polystyrene and polyurethane foam have enjoyed. The primary reason for this relatively slow growth is high process costs that result in an unbalanced cost/performance ratio. [13] History: The earliest patent, which was issued for the preparation of expanded polyethylene, was granted to Calendar’s cable and construction Co. Ltd. in 1945 and described the physical expansion of polyethylene using carbon dioxide. Other patents have been issued dealing with the physical expansion of polyethylene by using volatile liquids or gas pressurized into the polymer melt, with subsequent depressurization to produce cellular polyolefin. These processes were commercially not successful since they did not produce cellular products of acceptable cost/performance ratio. However, similar methods using volatile liquids or expanding agents have been successfully developed and commercialized. [13] Polyolefin Foams are a relatively recent development compared to the other types of foam. Polyolefin foam processes were developed in the 19605 and 19705. [32] Methods of preparations: In general, cellular plastics or composites based on polyethylene and polypropylene can be produced by both physical and chemical methods. Each process produces a specific 40 structure that depends on polymer properties, volume fraction present in the foam and cell morphology.[13] At present, there are four methods involving chemical foaming agents that are used commercially; 1. Direct extrusion expansion. 2. Compression molding using organic peroxides. 3. Pressure molding (Engelite and U.C.process) 4. Atmospheric expansion of radiation - cured sheet. Polyolefin foam properties; Low density chemically cross linked PE foam made by the high pressure molding process and by atmospheric pressure expansion of procured materials has been evaluated by Kadowaki and compared with other foams and found out that it is more flexible, strong and semi rigid than other foams. It has shock absorbing characteristics and water absorption is low than other plastic foams. It has a superior chemical resistance and electrical properties. It is harmless to human beings and does not corrode any surface metal. Polyolefin’s process ability is good. Cross-linking polyethylene has further advantages like Very foam uniform closed cells (1-6 mils). It has excellent esthetic appeal and acceptable heat insulation properties. Cross- linking polyolefin has a density as low as 1pcf. and an excellent ultra violet and weather resistance 41 1.5 MANUFACTURING METHODS FOR PLASTIC FOAMS There are many processes to make plastic foams. Selection of a process depends on many factors, for example 1) Quantity and production rate 2) Dimensional accuracy and surface finish 3) Form and detail of the product 4) Nature of material 5) Size of final product Typically, plastics processes have three phases: 1. Heating - To soften or melt the plastic resin 2. Shaping / Forming - Under constraint of some kind 3. Cooling - So that it retains its shape [8] The most common processes are injection molding and extrusion processes. A brief overview of these processes is given below. The most universal and efficient for creating a uniform thick and equally dense skin is the rotational molding or roto molding process. [3 ll 1.51 Injection molding . The most common way of producing foam parts is injection molding. Different classification systems exist. The classification described by Fydor A.Shutov [26] into four groups is mentioned below 1) Low pressure (LP) processes, up to 20 MPa 2) High pressure (HP) processes, up to 100Mpa or more 42 3) Gas counter pressure process and 4) Two- (or more) component processes. [26] Basic Principle. Plastic foam injection molding is similar to conventional injection molding. [26] Injection Molding is the process of forcing melted plastic in to a mold cavity. The part can be ejected after the plastic has cooled. Sometimes injection molding is used in mass- production and prototyping. Injection molding is a relatively new way to manufacture plastic foam. The first injection molding machines were built in the 1930's. [31] There are six major steps in the injection molding process: 1.Clamping An injection-molding machine consists of three basic parts; 1) the mold, 2) the clamping and 3) injection units. The clamping unit is used to hold the mold under pressure during injection and cooling. Basically, it holds the two halves of the injection mold together. [31] 2. Injection Plastic material in the form of pellets is loaded into a hopper on top of the injection unit during the injection phase. The pellets feed into the cylinder where they are heated until they become molten. A motorized screw within the heating cylinder mixes the molten pellets and forces them to the end of the cylinder. Once enough material has accumulated in front of the screw, the injection process begins. The molten plastic is inserted into the mold through a sprue, while the pressure and speed are controlled by the screw. Some injection molding machines use a ram instead of a screw. [31] 43 3. Dwelling, Cooling, Ejection The dwelling phase consists of a pause in the injection process. The molten plastic has been injected into the mold. Pressure is applied to make sure all of the mold cavities are filled. The plastic is then allowed to cool to its solid form within the mold. The clamping unit is opened, which separates the two halves of the mold. An ejecting rod and plate eject the finished piece (plastic foam) from the mold. Foam formation takes place following injection, either as a result of mold expansion or due to regression of plastic material from the mold. [26] 1.52 Extrusion Extrusion methods to produce plastic foams are readily available. The main advantages of these methods include continuous and high productivity, simple equipment and precisely sized articles. Solid and hollow profiles made of plastic foam can be successfully substituted for wooden articles (without any further machining) and profiles made of unformed plastics reduce feed stock consumption by 15 to 40 percent. Extrusion is particularly economical for fabricating finished articles that do not require any secondary processing. [26] Basic principle Extrusion occurs when a solid plastic (also called a resin), in the form of beads or pellets, is continuously fed into a heated chamber and the product is carried along by a feed screw. The feed screw is driven via drive/motor machine. Tight speed and torque control are critical steps in producing quality product. The product is compressed, melted, and forced out of the chamber at a steady rate through a die. Dies have been engineered and 44 machined to ensure that the melt flows in a precise desired shape. There is almost always downstream processing equipment that is fed by the extruder. Depending on the end product, the extrusion may be blown into film, wound, spun, folded, and rolled, and a number of other possibilities. [40] Plastics are very commonly extruded. Rubber and foodstuffs are also quite often processed via extrusion processes. Occasionally, metals such as aluminum are extruded plus trends and new technologies are allowing an ever-widening variety of materials and composites to be extruded at continually increasing through put rates. [40] Foam formation takes place when the polymer contains blowing agents which cause foaming at the extruder exit (or die) [26]. Figure 13 represents the basic extrusion machine structure. Basic Extruder Machine The feed screw, barrel, and temperature controller form a section of the extruder called the plastication unit. Plastication is defined as the conversion of a thermoplastic to a melt. This is critical to successful extrusion processes. [40] The major components in an extruder are following. Feed screw The job of the feed-screw is to move the resins through the barrel chamber in a steady and predictable manner. There are three main defined sections in a basic feed screw. The feed zone takes resin from the hopper and conveys it along. Resin pellets encounter friction from feed screw surfaces, barrel surfaces, and each other. This mechanical fi‘iction provides about 85% of the required heat, so it is critical that the drive equipment, which turns the screw, must have the HP (horse power) capabilities to overcome fiction 45 .‘l‘l and turn the feed screw at a steady and controlled rate. Some extruders can continue to plasticate materials long after their external heat sources are shut down. [40] The compression zone is next. The channel depth between screw flights diminishes and. the result is to pressurize melting resin. Friction, barrel heating, and compression complete the melting process. Two important design parameters are associated with this zone. ' The compression ratio is measured the channel depth at the end of this zone. Different compounds or operating pressures require different compression ratios. ' The length of the compression zone affects the rate of compression. These two parameters will be different for different compounds. [40] The metering zone has a constant channel depth and primarily exists to further mix molten resin. The end result is a smooth consistent melt with uniform temperature. [40] Devolatizing section. 4. In some processes, a de-gassing or devolatizing section is required. This is a shorter zone that immediately follows the compression zone (See figure 13). Channel depth is suddenly increased, and the resulting pressure drop causes a release of gas, which can be vented or drawn off via a vacuum pump. The remaining melt is re-compressed and metered. The following figure 13 show a basic Extruder machine. [40] 46 F -_ -1 ENE. Pr _ 1! Iii Figure No. 13 Plastic Hons industrial Camol Realm Hate Fumful / Screw u 2%; a... Euruda I // r Die Paws Um Elma Imam . Plait: ”PM | JL-IJ------:yr /Mmal T -' ' #Dmmln "l'""l"J_'.' ,. 511113131 _ __g___ /T min / ] ADPuanuinr II: MC It i . Basic Extuder Figure 13. Basic diagram of Extruder machine 1.53 Other processes a) Rotational Molding The most universal and efficient method for creating uniform thick and equally dense foam is rotational molding [26] In this process; plastic powder is scooped into a mold. The mold is rotated over a large gas burner. As the mold gets hot, the plastic melts and sticks to the mold. This method is used to make large hollow objects like water tanks and barrels. 47 b) Compression Molding Compression molding is used for thermoset resins. Dry powder is put in a mold, which is squeezed and heated until the plastic melts and cured. This is used for making ashtrays, cups and plates, and some electrical switches. c) Reaction injection Molding In this process, two chemicals are mixed together and squirted into a mold and the chemicals react together. This is used to they make car bumpers, some disposable cups and plates, and meat trays. d) Vacuum forming In vacuum forming process a sheet of plastic is clamped in a frame and heated until it becomes stretchy. It is then sucked into a mold. This process is used to make the inside of your refrigerator, bath and hand basin. It is also used to make a lot of packaging for cosmetics, chocolates, biscuits, some yogurt containers and disposable cups. e) Fabrication Some thermoplastics are fabricated like sheet metal. Sheets of plastic are cut to the desired shape. They can then be folded by heating a narrow line through the plastic. When it is soft, the sheet will bend along the heated line. Sheets can be joined together by gluing, or by welding. The joint is heated with hot air and a thin filler rod is forced into the gap. These fabrication methods are used to make acrylic signs and displays, and industrial tanks and equipment. They can also be used to manufacture laboratory fume cupboards and exhaust fans. Thin flexible plastic sheets are used for making folders, 48 ulz: wallets, swimming pool liners, inflatable toys and raincoats. The seams are welded using ultrasonic vibration. f) Styrene Foam. To make blocks of styrene foam, or complicated shapes like a cycle helmet, pallets are scoop into a mold and heated with steam. The steam makes the pellets swell and stick together. [1] 49 CHAPTER 2 MATERIALS AND METHODS Chapter 2 covers the material and methods section for the research “ Performance properties of biodegradable foam (Green Cell® foam) .The following M&M are presented 2.0 Twin Screw extrusion process 2.1 Cushioning characteristics 2.2 Dimensional stability 2.3 Moisture sorption 2.4 Thermal insulation 2.0 Green Cell® Foam is produced by twin Screw extrusion process Materials: The type of starch used was hydroxypropylated high amylose cornstarch (70% amylose content). The starch was purchased from National Starch and Chemicals (Indianapolis, IN), under the trade name of HYLON 7. The inherent moisture content of the starch was 11.2% under ambient conditions. Water was used as the plasticizer as well as the blowing agent. Water content was maintained at 7-10% of the starch used. Talc (Magnesium Silicate), used as the nucleating agent, was obtained from Luzenac (Ontario, Canada). It has a specific gravity 50 :1 7:1 of 2.76 and a bulk density of 150 kg/m’. The tale content was maintained at 1% for all the experiments. Poly (hydroxyamino ether) (PHAE) is an additive, which offers the adhesion and durability of epoxy resins with the flexibility and process ability of thermoplastic resins. PHAE was purchased from Dow Chemicals (Midland, MI), under the trade name BLOX 110. PHAE has a melt temperature of 75°C, and is produced by reacting liquid epoxy resin (LER) with hydroxy functional dinucleophilic amines and resorcinol diglycidyl ethers (RDGE) [45]. Experimental Setup: EQUIPMENT FOR GREEN CELL 1) Thick material. Twin Screw Co —Rotating Food Extruder: Wenger TX-80. (D=80 mm, L/D=20) 2) Positive displacement pump: For injecting water. 3) Screw Feedersl& 4) An Annular Die: 2.5mm width 5) Down stream equipment for cutting and rolling or laminating foam sheets. 6) Figure 2 represents a process flow diagram of making Green Cell foam. The experimental setup used in this study was a twin-screw extrusion system (fig. 14). The twin-screw extrusion system consisted of an extruder driver with a speed control gearbox, a Werner Pfleiderer ZSK-3O twin-screw co-rotating extruder with a screw diameter of 30 mm, an MD of 32, a positive displacement pump for injecting water into the extruder, accurate single-screw feeders for feeding starch, and PHAE and talc could 51 mmi WOUT {UHC 8351 The We.“ 3m. mhl be fed individually or as a mixture. A cylindrical filament die 2.7mm in diameter and 8.1 mm in length, with a cooling sleeve was assembled to the extruder. The sensors were mounted on the die to measure the temperature and pressure of the melt. A high-speed cutter was used to get cylindrical foam samples of required size. Basic principle The foam sheets are being produced on an industrial scale twin-screw food extruder, Wenger-80, having a screw diameter of 80mm and an L/D of 16. An annular die of width 2mm is used. Talc is not used in the production of starch foam sheets in order to get the minimum density product. Also, the addition of talc rendered the product more brittle. Water Figure 14. Process Flow Diagram of Green Cell Foam. [45] 52 of 2.1 Cushioning Characteristics of Green Cell® Foam. The cushioning characteristics of Green Cell Foam were deterrnrned, and compared with the G values of different plastic foams commercially available. The effect of relative humidity and time on the G value of Green Cell® foam was also evaluated. 2.11 Instrumentation (Lansmont drop tester) G value of one and two inch thick GCF were determined using Lansmont drop tester, (Monterey CA) at the controlled temperature 22°C and 50% RH .The instrument consists of the following components. 1) Instrumentation and shock sensors 2) A dropping platen The dropping platen must have a mechanism to attach additional mass for adjusting its total mass to a desired value. 3) Reaction Mass Reaction mass would be attached to the testing machine. Reaction mass would be sufficiently heavy and rigid so that no more than 2% of the impact acceleration is lost to the reaction mass while conducting dynamic tests. The reaction mass must be in contact with the ridged impact surface so that the two bodies move as one. 4) Accelerometer The accelerometer is a data storage system and is required to monitor acceleration versus time histories. The instrumentation system needs the following minimum requirements. Frequency response range from 2H2 or less to at least 1000Hz. 53 l: 71. Ci. ffi Accuracy reading to within 5 % of the actual value Cross axis sensitivity less than 5 % of full scale, and the instrumentation are required to measure the impact velocity to an accuracy of i 2% of the true value. Test material KTM Industries, Inc. develops, manufactures a bioplastic Green Cell® Foam. The type of starch used was hydroxypropylated high amylose cornstarch (70% amylose content). The . . . . . ® inherent morsture content of the starch was 11.2% under ambient conditions. Green Cell Foam is produced by twin Screw extrusion process. 25 pieces each of Green Cell® foam having dimensions of 8”x8”x1” and 8”x8”x2”were used. 20 pieces each of Green Cell® foam having dimensions of 6”x 6”x 1” and 6”x 6”x 2” were used 2.12. Methods. Conditioning The Material was conditioned at standard conditions (25°C and 50% relative humidity) prior to do the cushion testing. [3] Determining dynamic shock cushioning characteristics. The specimen was loaded onto a rigid plate or onto the machine platen to 0.025 psi (17.55 kg/mz) on the top surface area. After a 30 sec interval, the thickness to an accuracy of 1/32 inch was measured by averaging the thickness measurements of the four corners of the specimen. This value was recorded as the specimen thickness. 54 The top surface area of the specimen was measured with an apparatus yielding values accurate to 1/32 in. The mass of the specimen was measured with an apparatus yielding values accurate to 30g. [3] The test specimen was centered on the impact surface face and the platen was positioned to strike the cushion on its top surface area. The specimen was subjected to a series of five drops at a pre-deterrnined static loading and impact velocity allowing a minimum of 1 min between each drop. A complete acceleration time record for each drop was recorded and the impact velocity of the platen was measured just before impact to ensure that it was representative of the impact velocity equated to the desired free drop height. To obtain dynamic data for a given cushion, it is necessary to repeat the five test drops on new specimens varying some aspect of the test such as static loading impact velocity or cushion thickness. [3] 2.13 Calculation The density of a test specimen was calculated using the following equation. D = (3.81x M)/ (leszT) D= density (1b /ft3) M = mass of the specimen (g) L1 = length of the specimen (in) L2 = width of the specimen (in) T = original thickness of the specimen in 55 For free fall height, the following equation was used H = Vi2 /2g and impact velocity can be calculated using the following equation. Vi = \/2gh H = free fall drop height (in) Vi = measured impact velocity in/sec G = acceleration due to gravity 386 in/sec2 Dynamic set can be calculated using the following equation Dynamic set % = [(T-F)/T] x 100 T = original thickness of the specimen (in) F = thickness of specimen after test (in) [3] 2.14 Effect of % RH and temperature on C values Method. To determine the effect of relative humidity on GCF ’s G value, 2- inch thick material was tested to determine its G value according to ASTM standards D-1596. Seven pieces of GCF were determined based upon 1St impact and then these seven pieces of Green Cell® 56 foam were held under seven different relative humidity conditions at 30° C for two months. After two months, GCF pieces were again tested to determine their G value at the same static load, drop height and weight. _ 2.15 Effect of Time on G values. 1-inch thick material and 2-inch thick material were tested at different times during three months of storage. The G value of l-inch foam was 80.80(average) initially. The same batch of material was then tested after two months at ambient conditions (humidity and temperature conditions varied according to the external weather conditions). 2"° set of fresh material was then received and was tested again to determine the G values at same the drop height, bearing area of foam and static load. Fresh material had a G value of 80.804(average of five drops). 57 Ed I) 2.2 Dimensional Changes Dimensional changes (length, width and thickness) of GCF and net weight loss /gain of the product (Green Cell®) at 30°C/ several different humidity conditions was determined. An experiment was set up using samples of Green Cell® foam and saturated salt solutions. Salt solutions were prepared according to ASTM standard E104 [2]. Detailed can be seen in appendix E. Dimensional changes and weight loss/gain were measured periodically until equilibrium conditions were achieved. Effects of ambient conditions on GCF were also determined. Materials and Methods, Materials. Dimensional changes at different relative humidity (%RH) conditions and 30°C I 14 pieces of Green Cell® Foam having dimensions of 2”x 2” x 1” I Seven RH chambers I Digital vemier caliper (supplies) Material behavior at ambient conditions I Three pieces of Green Cell foam having a dimension 5 of 8” x 8”x 2” were used to examine the Green Cell® behavior at ambient conditions. Change in thickness under load I Several pieces of Green Cell® foam having a dimensions of 8”x8”x2” and 8”x8”x1” were used. to examine the effects in thickness under load conditions. 58 I Vernier caliper I Dematerialized water I 8 one gallons of bottles I 8 wooden blocks 8”x 8”x '/2” Methods: Dimensional changes at different relative humidity (%RH) conditions and 30°C. Salt solutions were prepared according to ASTM standard E104 (Appendix E). Green Cell® foam material was cut into 2x2xl inch pieces. The dimensions were measured using a digital vemier caliper and weight was measured using an analytical balance. All the pieces were placed into the HDPE buckets containing different salt solutions to create specific humidity conditions. All the HDPE buckets were placed inside an environmental chamber at 30°C. Each piece was marked as to its length width and thickness. Dimensional change in each piece was measured by vemier caliper and weight was checked by analytical balance each day for the first week and then at a time interval of 1-3 days until the weight of the product became constant. Each piece was marked at one specific location when taking the first reading and all subsequent readings were taken using this as reference. One piece of material was removed from the bucket and measurements, at a time, measured quickly as the product is sensitive to moisture. Latex gloves were used to avoid any contamination or hand moisture. 59 Material behavior at ambient conditions. 1” and 2” Green Cell® foam was kept under observation in. the experimental lab where temperature and relative humidity conditions change according to the weather conditions for about three months. The Change in thickness of Green Cell® Foam under Specific load a) At 50%RH and 25°C b ) At ambient conditions Two sets of experiments were conducted to determine the change in thickness under load. One set of experiments was conducted in a room where temperature and relative humidity conditions varied according to ambient conditions. Another set of experiments was conducted in a controlled conditioned room where temperature and relative humidity conditions were maintained at 25°C and 50% RH. One gallon Plastic bottles were filled with water and placed on top of the Green Cell® foam pieces which had been covered with wooden blocks. Wooden blocks were placed over the Green Cell® foam to provide uniform weight distribution over the foam pieces. Thickness of GCF was measured periodically with using a digital vemier caliper. Thickness was determined at the same location each time to minimize error. 60 2.3 Sorption isotherm Sorption isotherm was developed at different RH% conditions and net weight changes at 30°C and different RH %conditions were measured. 2.31 Sorption isotherm at different %RH and 20°C,25°C and 30°C 2.32 Net weight changes at 30°C and different %RH conditions 2.31 To determine the moisture sorption isotherm of the product at 20°C, 25°C 30°C Empty aluminum dishes were weighed and approximately 0.5-2 grams of product was added to each dish. Green Cell® foam was cut into small pieces to increase the surface area of the product to allow it to reach equilibrium conditions. Dishes were reweighed. Triplicates were prepared for 7 or 8 humidity conditions. Aluminum dishes containing GF C were then placed over saturated salt solution prepared at different relative humidity conditions. Three replicates were prepared. Storage temperatures used were 20°C, 25°C and 30°C.Weight readings were taken every day for the first week, then at a time interval of 1-3 days until the weight of the product became constant. The equilibrium moisture content of the samples, was determined using the following formula:[18] Me We W,(M,+l)-1 Where, 61 We, Equilibrium or final weight of the product Wi_ Initial weight of the product Mi. Initial moisture content of the product Sorption isotherms were then plotted at the three temperatures used GCF. The GAB model was used to obtain the best fit for the product. Graphs were plotted between aw/Me and Me to obtain various constants (a, [3, y) for each temperature to develop the GAB model. Comparison was made between experimental values and the GAB model values. RMS values were then calculated. The best fit was determined using the RMS value, the lower the RMS value, the better fit. Determination of the Initial Moisture Content (Mi) of the product by Gravimetric method: Initial moisture content was determined using the AOAC official method 934.06. as modified. [4] Three empty aluminum dishes were weighed and 1-2grams of product added and reweighed. The product was then placed in a Laboratory National vacuum oven at 75- 80°C under 22-25in Hg for 8-9 hours to determine the moisture loss from the product. Initial moisture content of the product (dry basis) was then calculated using the following formula: [4] Initial Moisture content of the product = Wi-Wd x 100 Wd Where, 62 W: = initial weigh of the product Wd = Final weigh of the product 2.32 Net weight changes Salt solutions were prepared according to ASTM standard E104 [2]. Detailed calculations can be seen in appendix E. Green Cell® foam material was cut into 2 x 2 x 1 inch pieces. The weight was measured using an analytical balance. All the pieces were placed into the HDPE buckets containing different salt solutions to create specific humidity conditions. All the HDPE buckets were placed inside an environmental chamber at 30°C. Weight was checked by analytical balance each day for the first week and then at a time interval of 1-3 days until the weight of the product became constant. One piece of material was removed from the bucket and measurements were taken quickly to avoid extra moisture absortion/desorption. Latex gloves were used while taking the reading to avoid any contamination or hand moisture. 63 2.4 The package insulating ability (R -Va1ue) and bulk density of Green Cell® foam. A modified version of ASTM D3103 (ice melt method) [10] was used to quantify the insulating ability of a package by specifying a means for calculating its thermal resistance (R -value). Density of the foam was calculated .In order to calculate the R- value R- value, a cooler measuring 11 x 10 x 9 ”8 inches was fabricated from GCF and used as the test specimen. EPS and Green Cell® coolers were made to have the same dimensions. To compare the R- value of Green Cell® with EPS, experiments were performed at the same time, in the same environments with the same equipment and the same amount of ice. Experiments were performed in two different environment, 30°C and 80% RH and 25°C and 50% RH. [5 a ] 2.41 Materials. I For density calculations three pieces of Green Cell® foam having dimensions 8”x8”x2” and three pieces of Green Cell® foam having dimensions 8”x8”x 1 ”were taken. I Ruler I Analytical balance I Ice Melt method [10] Regular cubed ice or crushed store ice can be used. The amount of ice was used was based on the available inside volume of the coolers (EPS and GCF). Approximately, 1/2 of the inside volume was filled with ice. I Package: 64 I Green Cell® cooler. A GCF cooler was made by using couurugated fiberboard as a frame. Hen placed into the fiberboard Slabs of GFC were then placed into the fiberboard box. I b) EPS Coolers: An EPS cooler was made of l l’Q-inch thick EPS foam. I Bucket: Plastic buckets was used the coolers it. Metallic buckets can interfere with the calculation of the package R-value by providing a reflective surface not associated with the coolers itself. Same size and same color buckets were used for GCF and EPS coolers. I Duct tape or any sealing adhesive tape: Sealing is a very important step. Stray air currents can flow in and out even through the smallest of openings. This can carry enough heat to render the best insulator ineffective. I Ruler: to measure the dimensions. I Thermometer: graduated cylinder or weight scale [10] 2.42 Methods Density of the Green Cell® Foam: Density of Green Cell® foam were calculated .Two Green Cell® foam dimensions were used to determine it’s density, 8”x8”x2” and 8”x8”x1”. Weight of the material was measured using an analytical balance. Length, width and thickness were measured using a measuring tool (ruler). Averaged density was calculated from three replicates. 65 Calculation The density of the specimen was determined according to the following formula D = (3.81x M) (leszT) D: density (lb /ft3) M = mass of the specimen (g) L1 = length of the specimen (in) L2 = width of the specimen (in) T = original thickness of the specimen in R-value Ice Melt method. This test closely resembles the situation in which an insulating container would be used be used & it is also similar ASTM D3103: Standard Test method for thermal Insulation Quality of a Package [10]. In the ice melt test a quantity of regular cubed or crushed ice is placed in a non— metallic bucket (preferably plastic made of HDPE) inside the package. The package was sealed with duct tape to avoid any air circulation from the outside environment into the package or vice versa. This assembly was stored at 50%RH and 25°C (77°F). A second trial was done at 80% RH and 30°C (86°F). The amount of ice used, was selected to fill at least 66 half of the available volume. The ice was then allowed to melt for several hours, after which the bucket was removed, and the water drained out and discarded. This was a preconditioning procedure intended to ensure that the ice was uniformly at its melting temperature, (32°F) before the actual test would begin. This then maintained a constant temperature difference across the package wall. Metallic buckets must not be used because they could interfere with the calculation of the package R value by providing a reflective surface not associated with the package itself [10]. The buckets were then placed back inside the package near the center and the package was sealed with tape to make it relatively airtight. Sealing is very important. Stray air currents may flow in and out through the smallest of openings and carry enough heat to render even the best insulator ineffective [10]. The day and time were recorded and the package was immediately placed in a draught free constant temperature environment, at 50% RH and 25°C, on a shelf or other surface off the floor. The package was then allowed to sit in this environment for at least one day and possibly two or three days depending upon the package. The aim is to get most, but not all, of the ice to melt. The experiment was replicated three times as specified in ASTM [10]. The day and the time were recorded at the end of this time period. The box was opened, the bucket removed, and the water was drained out. The water collected during this procedure was weighed, since it takes 144 Btu of heat to melt 1 lb of ice (the latent heat). The heat transfer rate in Btu fh into the package was the melt rate multiplied by the latent heat. This can then be depicted as a system R- value using the following formula. 67 System R- value = (box area) (Temperature difference) (Melt rate) (Latent heat) The R- value mainly depends on the wall construction, and not the size of the package and is a reciprocal of the effective coefficient of heat transfer. The box area term is the inside surface area of the package. The temperature difference term is the temperature difference between the outside air and the ice. The melt rate term is the rate at which ice melts during the experiments and is equal to the weight of the water (melt ice) collected divided by the exposure time. The same experiment can be done with dry ice (solid C02). Since dry ice goes directly from a solid to a gas, the melt rate would be calculated as the difference between the starting & ending weights of the block of dry ice, divided by the exposure time. The temperature difference must be based on an ice temperature of —180.4°F instead of 32°F, & latent heat of 240 Btu/lb instead of 144 cal. Whichever method is used the R- value should be the same [10]. The summary of research on the performance properties of Green cell Foam (GCF) can be seen in figure no. 1 5 68 Research overview Performance properties of Green Cell U ' E B F to 31' a. Cushioning Dimensional Sorption R- Value Effects Changes Isotherm G Value at 25“C and Dimensional Different R11 and R-Valuc at 25°C and 50%RH Changes at 20.25 50% R11 Different R11 and and 30"C 30°F Comparison of GCF Atmospheric Effects Net weight Changes R- value at 30“(‘ with at And 86% RH other plastic foam 30C and different "AR" Time Effect on G Changes in Ihickness l \"alue under load %RH and At Temperature 50%RH Effect on (i \alue And 25"(' Atm Fond. Figure No 15. Overall Research overview of the Performance properties of Green Cell Foam. 69 CHAPTER 3 RESULTS AND DISCUSSION The results and discussion are divided into different sections as follows. 3.1 Cushioning characteristics 3.11 G value at 25°C and 50%RH and comparison of G values 3.12 Time Effect on G values 3.13 Effect of relative humidity on G value 3.2 Dimensional stability 3.21 Dimensional changes at different relative humidity (%RH) conditions and 30°C 3.22 Material behavior at ambient conditions 3.23 Changes in thickness under load 3.23-a at 50%RH and 25°C 3.23-b at ambient conditions 3.3 Moisture sorption 3.31-a Sorption isotherm at different %RH and 20°C, 25°C and 30°C 3.3 l-b Net weight changes at 30C and different %RH conditions 3.4 Thermal insulation 3.41 Density calculations 3.42 R- value at 25C and 50% RH 3.43 R- value at 86%RH and 30C 70 Results and Discussion 3.1 Cushioning Characteristics of Green Cell Foam. The cushioning characteristics of Green Cell® Foam was determined and the G values of Green Cell® foam were compared with the G values of different plastic foams commercially available. Effect of relative humidity and time on the G value of Green Cell® foam was determined. Packaging designers face many challenges in predicting the performance of cushioning materials, when designing protective package .The prime objective is to choose the proper cushioning material that will protect the product from the hazards of the distribution environment, such as shock and vibration. It is also to achieve the most cost effective package. Classically, shock attenuation characteristics of cushioning material have been considered a material characteristic. Shock attenuation is commonly presented as a cushioning curve, which is a plot of peak acceleration in G’s vs static loading and is used to compare and qualify materials. [41] Peak acceleration is represented by G; such forces are basically a shock of very short duration, and high deceleration. [42] By definition, deceleration is the rate at which an object slows down, and can be written as G = deceleration g 71 G is a dimensionless number and important in designing a package because it is proportional to the impact force on the product and impact force is what damages the product [42]. Fundamental information about the product is necessary to develop a precise and low cost package for product protection. Thus, fragility level is the most vital parameter to determine. [41]. Gorman [41] defines fragility as “The maximum acceleration and velocity change the product can withstand before damage occurs”. Typical fragility levels for different products is presenting in the following table 2 [42] Extremely Missile guidance systems, precision aligned test 15-25 G’s fragile instruments. Very delicate Mechanically shock mounted instruments and 25-40 G’s electronic equipment, Disk drives. Delicate Aircraft accessories, Computers, Laptops, Flat 40-60 G’s Panel monitors, Standard Monitors, Printers, Scanners. Moderately Television Receivers, Aircraft accessories 60-85 G’s Delicate Moderately Major Appliances 85-1 15 Rugged G’s Rugged Industrial Machinery 115 G’s and above Table 2. Typical Fragility Levels for Different Products [42] 72 This information is then charted to form a damage boundary curve (DBC). A Damage boundary curve is drawn between the critical. velocity change (AV) and critical acceleration (AG) and is obtained from drop tests. From the DBC curve, the fragility of the product can be determined. [11.]. Classically, cushion curves are used to identify a material thickness and loading range based on a pre-determined drop height and required acceleration level. By comparing cushion curves of various materials (generated using the same test method), a cushioning material with the least amount of surface area and thickness can be chosen [41]. Cushion characteristics can be determined by plotting cushion curves. A cushion curve is a graphic representation of a transmitted shock (G) over a variety of static loading conditions (psi or kg/m2) for a specific cushioning material thickness at a specific equivalent free fall drop height [11]. G values of the Green Cell® Foam (two inch and one inch thickness) were determined at different static stresses (psi) by keeping the same drop height (24- inches) and then comparing these G values for the same thickness and drop height with commercial foams (tables 3 and 4). It was also found that GCF could not bear the total reaction mass 63.3le. Green Cell® Foam tore as shown in the figure 16. 73 Figure 16. Material damage at 1.75psi, determine G value, 1St impact Table 3: Comparison of the G value of Green Cell Foam® two inch thick with the G values of commercial materials.* (2” thickness,24 in Drop height) [5-a] Static 74 The G values of commercial material were taken from the literature [15]. At lower static stress, Green Cell® foam had low G values as compared with the other materials while at higher static stresses the material behave about the same as the market competitors [5-a]. This results shows that G values of 2-inch thick Green Cell foam is competitive with the other foams as for as G values are concerned. Graphical representation of the comparison of the G values can be seen in figure 18. G vs ststic stress(2-inch thickness) 45 40 .-.. -- -- ..-v. .WJ. ‘l 35 __- , ’ We .1 ,_ , -- 30 T T T" ”‘27" "WT“ ":lggE'Gg 25 — . - -- -_ -- ,_----,_ , , . 20 -—--— -, W — .- 15 -~ , - ~ . 1° [*GCF -ffi, . M ] G's 0 0.5 1 1 .5 2 Static stross(psi) Figure 17. G values of Green Cell® foam Vs Static Stress (psi) * 2-inch thick GCF 75 Comparison of G values 2" thickness 80 70 ]— °° ’” +PE ,G's i; 50 ~ -—— +GC ,G'e o +EPS,G'e , 2 40 -_ g EPE(Dow) o 30 r _ +EPE(Arco) ‘ 20 i- - - _ - -__ - __-_ _ ,_. _ _-O—EPE(D9wL 1o 0 o 0.5 1 1.5 2 Static Stress(psi) Figure 18 Comparison of the G values of 2 in thick GCF with the G values of commercial materials. * (2” thickness 24” Drop Height) 1-inch thick Green Cell® foam was also tested to determine its G values and these values were compared with the G values of other foams. At lower static stress, Green Cell® foam had lower G values as compared with other materials, but at higher static stress, had higher G values as compared to the competititive foams [5-a]. This comparison can be seen in table 2 and graphical representation is shown in figure 19. 76 Table 4. Comparison of the G values of Green Cell® foam with the G values of other commercial materials(l” thickness 24” Drop Height). PE (1.25pcf) (220ch (2.2pcf) (2.2pcf) Green Cell Static stress G value EPS EPE(Dow) EPE(Arco) Dow (3.4pcf) S.S psi PE ,G's EPS,G'5 EPE(Dow) EPE(Arco) EPE(Dow) GC ,G's Stdev 0.2 120 116 81 92 100 56.6 4.6 0.355 105 87 65 81 64 63.0 1.1 0.403 73 8O 63 73 63 72.0 3.1 0.8 64 63 59 95 60 81.0 1.2 1.305 75 65 90 73 117.0 0.0 1.44 83 70 97 80 116.0 4.5 1.58 90 78 105 83 117.0 2.0 1.722 105 84 110 87 131.0 1.6 Graphical representation of the comparison of the G values can be seen in figure 19. 77 Comparison of 6 values 1" thick foam 140 120 . 100 . - PE .6'3 9 —I— GC ,G's 9 so - g +EPS,G'e E 60 , EPE(Dow) a —I— EPE(Arco) 4o 4 -_- —— - — W W W W- - |W3—EPE(Dow)7 20 a. _ _ - _ _ -- #_ 7 + W- __-- 0 W 0 0 5 1 1 5 2 Static Stross(psi) F ig19. Graphical representation of the G value of ‘Green Cell® foam with the G values of other commercial materials. *(1” thickness 24” Drop Height) G vs static stress(1-inch thickness) 140.0 120.0 -—er -__- WWW W a O ‘ 100.0 -W W -W—- __,-_, .- .. _ . _------ 80.0 -_ .._-.--- _.‘ __ -----,,--___- f - . I 60-0: ---- —---W W — _-_-_- .e-__- m 40.0 W WW . . WWW -.-_.-_-_-- 20.0 W- __ - - .- ..__-_ . ________._. _- 0.0 G's L Static Stress (psi) Figure 20. Graph between G values of GCF Vs Static stress (* l-inch thick GCF) 78 3.11 Effect of Time on G values: The G values of GCF decreased with time. l-inch thick material and 2-inch thick material were tested at different times during three months of storage. It was observed that the G value of l-inch foam was 80.8(average) when material was received. The same batch of material was tested two months later. The material was kept in an ambient air-conditioned environment where humidity and temperature conditions varied according to the weather conditions. The G value was found at that time to be 51.6. A 2nd set of fresh material was then received and tested to determined the G values at same the drop height (24 inches), bearing area of foam (64 inz) and static load (51.0 lbs). Static stress was kept constant (0.8lpsi). The fresh material had a G value of 80.8(average of five drops This behavior can be seen in table 5. Table 5: Comparison of G value of *GCF with respect to time Thickness 1- inch Green Cell® foam Type of material C value s.dev Fresh material lSt set 80.0 2.2 Two months later-1St set 51.7 3.3 Fresh material 2nd set 50.3 1.7 Two months later-2nd set 80.8 2.2 79 Similarly, two-inch thick foam was tested and showed the same pattern. The first set of fresh material was tested and had a G value of 34.9 with the st. dev of 3.8. It was then kept at ambient conditions where temperature and humidity conditions varied according to the weather conditions. Two months later it had a G value of 24.2(st dev. 1.3). A 2"d set of fresh material was tested at the same drop height (24 inches), bearing area of foam (64 inz) and static load (51.001bs). Static stress was kept constant (0.81psi). Fresh material had a G value of 35(average of five drops) with the st.dev of 1.02. 3.1 2 Effect of relative humidity on G value: Relative humidity had a significant effect on the G values of Green Cell® foam. Green Cell Foam® at 11% and 43% had an increased G value (from 39.97 to 51.84) and (from 43 to 45.2) [S-a]. No significant increase in weight was observed. There was no distinct change observed in G values at 54%, 75%and 86% RH. But at 89%RH and 96% RH, an increase in G values were observed along with Significant increase in weight [5-a]. Expansion in the thickness direction was observed at 75% RH, 30°C. This behavior can be seen in figure 20. Fungus was also observed on the material at 89% RH and 96% RH, contracted significantly and lost its shape. The bearing area of the Green Cell® foam decreased. As toughness and bearing area decrease, G value increases. These results are shown in the following figures (21-30) and tables. (6 and 7) Detailed calculations and material physical changes are shown in appendix A 80 Table 6. G value and change in weight (Aw) of Green Cell® foam with respect to time. if Two Fresh Two months Fresh months material later material later Aw s.no RH G value G value wt. wt. met wt. gaim % (g) (g) (g) 1 11 39.97 51.84 51.62 52.68 1.06 2 43 38.58 45.21 52.65 52.64 -0.01 3 54 32.18 38.29 54.58 54.7 0.12 4 75 39.22 36.53 51.86 53.96 2.1 5 86 32.9 37.25 56.34 62.03 5.69 6 89 39.15 50.63 51.51 60.59 9.08 7 97 38.42 76.77 52.38 67.31 14.93 Table 7: Comparison of impact time and impact velocity before and after keeping the material at specific %RH conditions. l—\ Fresh Two months Two months material later Fresh material later JJlo RH time time velocity velocity % (ms) (ms) (in/sec) (in/sec) l 11 22.8 17 177.25 182.63 2 43 23 18.1 170.57 174.4 3 54 25.2 21 158.19 171.59 \4 75 22.9 22.6 172.57 169.08 \5 86 25.8 18.8 164.47 153.64 \6_ 89 22.1 16.4 169.92 163.43 \7 97 22.8 12.4 169.86 184.1 81 Figures 21-30. Show the Green Cell Foam kept at 25°C/ 50%RH, at 30° C 75% RH,30 °C /84%RH,30 °C /89%RH and 30°C /96% RH. 25°C and 50% RH 30°C and 75% RH Figure 21 (Front view) Comparison of Green Cell® foam kept at 25°C, 50%RH and 30°C, 75% R 25°C and 50% RH 30°C and 75% RH Figure 22 (Side view) Comparison of Green Cell® foam kept at 25°C, 50%RH and 30°C, 75% RH [5'3] 82 25°C and 50% 30C and 84% RH Figure 23. (Side view) Comparison of Green Cell® foam kept at 25°C, 50%RH and 30°C, 84% RH Material became soggy, lost its shape and And showed marks of deterioration 83 Figure 24 GCF kept at 84% RH and 30°C 25°C and 50% 30°C and 89% RH RH Figure 25 (Front View) Comparison of Green Cell® foam kept at 25°C, 50%RH and 30°C, 89% RH [5-a] Fungus growth 84 Figure 26. Material kept at 89% RH and 30°C l 25°C and 50% RH 30°C and 89% RH Figure 27 (Side view) Comparison of Green Cell® foam kept at 25°C, 50%RH and 30°C, 89% RH . 2." i 25°C and 50% RH 25°C and 50% RH 85 Figure 28 (Front view) Comparison of Green Cellq‘ foam kept at 25°C, 50%RH and 30°C, 96% RH Fungus Growth Figure 29. Material kept at 96% RH and 30°C 25°C and 50% RH 30°C and 96% RH Figure 30 (Side view) Comparison of Green Cell® foam kept at 25°C, 50%RH and 30°C, 96% RH 86 3.2 Dimensional stability The dimensional stability of Green Cell® Foam was determined. Dimensional changes (length, width and thickness) and net weight loss /gain of the product (Green Cell®) at 30°C and different humidity conditions were determined. Dimensional changes at 30°C at several % RH conditions A 4.3-6.0 kg weight was placed on the material and changes in thickness were observed periodically. An experiment was set up using samples of Green Cell® foam and saturated salt solutions. Dimensional changes and weight loss/gain were measured periodically until the equilibrium conditions reached. Change in thickness: The most expansion accrued at 75% and 84% and this behavior can be seen in Figs 21- 25. The material expanded 0.400 inches during 408 hrs at 84% RH and 30°C, and 0.332 inches during 408 hrs at 75 % RH and 30°C [5-a]. Detailed calculations are shown in appendix B-Dimensional Changes. Negligible change in thickness was observed (0.03-0.075 inches) at 11%, 43% and 56% RH% at 30°C.The material contracted slightly ((—0.053, - 0.055) inches) at 89%RH and 95% RH%. 87 ,_ ka Saw-(3'4 F” *9 7°, ” a “z‘aixf 7m MN Ti gi i.” ”‘15-'11“: Figure 31. Comparison of GCF maintained at 84% RH/30°C and 50%RH /25°C. (Front view) 84% RH/ 30°C ‘n' i -. RH 8117. _ "WME One. WEEK! Figure 32. GCF maintained at 84% RH/ 30°C and 50%RH /25°C GCF pieces were compared afier one week of time period. (Side view). 88 "Vb 50% RH and 25°C 75% RH and 30°C Figure 33. Comparison of samples maintained at 75% RH/ 30°C and 50%RH/25°C. (Side View) 50% RH and 25°C i 75%RH and 30°C Figure 34. Comparison of samples maintained at 75% RH/ 30°C and 50%RH /25°C. (Front View) 89 Net Change in thickness 0.6000 :5. 0.5000 w W W _ 3 04000 _ “ml-‘5 .. T 11%RH E ' I ‘ “'. ;—I—43%RH g 0'3000‘” *’ ‘11 I fl * ’ “f0 l 56%RH ‘E 0.2000 -- 11L W 7, W 75% RH E, 0.1000 — r .. .. _. .. .. —W 1+34%RH "é“: ‘si‘hé— +39%: ‘ ~‘ - —+—— 5 §-o.1ooo W |— R» ‘9'Q!'n_ 0 l +° C -0.2000 7 Time (hrs) Figure 35. Net Change in thickness of GCF at 30°C at different humidity conditions Width: Significant change in width was observed at 89% and 95%. Material shrunk in the width dimension (—0.60 inches and -0.50 inches) at these two RH% conditions. At 84 % RH, material contracted in the width dimension slightly “ —0.132 inches”. At the remaining, RH% conditions (11%, 43%, 56% and 75%), only slight (0.02- 0.04 inches) change was observed. in width during the storage study period. Change in width can be seen in the following graph. 90 Net Change in Width at 30C 0.2 .73: 0'1 flrfim —I 7* __ ¢_ ¢ _; I E o 37...... =— . WWW—— +11%RH §-0.1'WW W m Wu W--: W -m - 500 +43%RH‘ 5-02. WWW W W WWW W - W 56%RH '; -o_3 _ ‘ __ 1 W 75% RH €044 ‘ ~ ~ ~ , '—x—-84%RH* -= -o.5 - W '\§‘ ‘ W +89% RH o .6 _0_6. . M’ s ..- s, - +95%.RI1 z -o.7W W WW W ~ -0.8 Time(hrs) Figure 36. Change in width of GCF at 30°C at different humidity conditions. Length Significant change was also observed in length at higher humidity conditions (95% and 89%). The material shrunk almost 0.90 inches in the length direction. At 84%RH material contracted in the length direction only 0.23 inches. This behavior of the material can be best seen in figure 6. No significant change was observed at 1 1%, 43%, 56% and 75% RH. 91 Net Change in length at 30C 0.2000 A T C 2. 0.0000 I 7 * +11%RH '- 1 500 _ 2’ 02000 W ”43% R“ 2 56% RH § 04000 — 75% RH g +84%RH g '0-5000’ ‘—o—89%RH ‘5 -0.8000 W +9§%,RH C 4.0000 1 Time(hrs) Figure 37. Change in length of GCF at 30°C and different humidity conditions. Figure (a) 50%RH and 25° C 95%RH and 30°C 92 Figure (b) 50% RH and 25°C 95% RH and 30°C Figure No.38 (a and b): Comparison of GC F samples kept at 95% RH, 30°C and 50%RH and 25°C. (Front View) 3.21 Material behavior at ambient conditions: 1” and 2” Green Cell foam was kept under observation in an air conditioned lab but not controlled where temperature and relative humidity conditions changed according to the weather conditions for about three months. Physically it was observed that material increased in thickness. This behavior can be seen in the following figures 39 and 40. 93 Fresh GC F sample Three months Old GCF (2- inch thickness) sample (2- inch thickness) Figure 39 (side view). Comparison of 2” fresh and three month old GCF material [5-a] Fresh GCF sample Three months Old GCF ‘ (1- inch thickness) sample (l- inch thickness) Figure 40. Comparison of l-inch fresh and three month old material 94 3.22 The Change in thickness of Green Cell® Foam under constant load at controlled conditions (50% RH and 25° C) The effect of load over time on the thickness of GCF was also determined. Both l-inch and 2- inch foams decreased slightlyover time under load at 25 °C and 50%RH. No significant change was observed during the storage period in thickness under load. A weight of 4.3-4.5 kg weight was placed on the top of the foam pieces for 53 days. Only 0.0230 inches of net change in thickness was observed for 2-inch thickness material during the storage period. While only 0.068 inches decrease in thickness was observed for 1-inch thickness material. No physical, change was observed during the study period. This behavior of material can be best seen in the following figures and tables Table 8. Relationship between change in Thickness under load at 25°C and 50% RH ( 1- inch thick sample) Time Thickness Thickness Thickness Average days (i_n) (in) (in) thickness 5 dev 0 1.23 1.1965 1.2455 1.2240 0.03 1 1.205 1.1865 1.208 1.1998 0.01 2 1.209 1.208 1.223 1.2133 0.008 4 1.1885 1.1905 1.155 1.1780 0.02 6 1.188 1.176 1.145 1.1697 0.02 8 1.187 1.1725 1.144 1.1678 0.02 10 1.2245 1.1925 1.1715 1.1962 0.03 12 1.2035 1.174 1.1685 1.1820 0.02 15 1.2065 1.1955 1.1785 1.1935 0.01 17 1.171 1.1605 1.147 1.1595 0.01 19 1.202 1.1635 1.1645 1.1767 0.02 27 1.172 1.1495 1.164 1.1618 0.01 35 1.179 1.152 1.186 1.1723 0.02 48 1.1535 1.1385 1.1735 1.1552 0.02 Net change -0.0688 95 thickness under load 1.2600 . 1.2400 1.2200 1.2000 1.1800 1.1600 1.1400 1.1200 0 thickness Thickness(ln) R2 = 0.5239 0 10 20 30 40 50 60 Time(days) Figure 41. Graph of Time (days) Vs Thickness of Green Cell® foam (1-ich thick GCF) at 25°C and 50%RH at constant load Table 9. Relationship between change in Thickness under load at 25°C and 50% RH (* 2-inch Green Cell® foam) Time Thickness Thickness Thickness Average 2.2324 2.0695 2. 2. 06 1 2.2412 2.1255 2. 1 2.134 2.1 2.1605 2. 2.1335 1245 2.1 2.15 2.1125 2.1165 2.1215 96 2.30000 Thickness under load 2.25000 2.20000 ‘ 2.15000 4 Thickness(in) 2. 1 0000 2.05000 — 2.00000 0 20 4O Time(days) E 0 thickness Figure 42. Graph between Time (days) Vs Thickness of Green Cell® foam at 25°C and 50%RH at constant load(* 2-inch Green Cell® foam) Combined results of 1-inch and 2-inch thick Green Cell® Foam can be seen in figure 43. 2.4000 , 2.2000 W .T 3;: I4; -__ T__ ”T 1i {1- ’5 1E1 E i 1 2.0000 - WW- WW W. -.-._ . ,. 1.8000 ~— , *2_. 1.6000 WWWWW W k - 2- “if _ I 1.4000 «- W 1 1.2000 Wish ‘37- “i .32! 2W 1.0000 0 10 20 30 40 50 60 +— E + L, 1" thickness 1 axe.thickness ' 2" ave.thickness l 1 1 Figure 43. Change in thickness under load at 25°C and 50%RH for 1 inch and 2-inch GCF 97 3.23 Change in Thickness under load at ambient conditions: Not significant change was observed during the storage period in thickness under load at ambient conditions. This experimental set up was placed in air-conditioned room but not controlled conditions (temperature and relative humidity conditioned varied). Total 5.9 kg weight was placed over the foam piece. Experiment was kept in progress for 23 days. Inconsistence decrease and increase in thickness was observed during the observation/study time. Only “-02.0 inches” of net change in thickness was observed for 2- inch thick GCF sample on the 24th day. While total 0.023 inches change in thickness was observed on 24th day of storage study for the 2- inch thick GCF sample, which was kept at controlled conditions (50% RH and 25°C). Physically appearance of the foam was detoriated, material become soggy (because of absorption of moisture from the environment) and slight change of shape was observed. This behavior of material can be best seen in the following figure and tables. Table 10. Relationship between change (A) in Thickness under ambient conditions. (* 2-inch Green Cell® foam) thickness(in) 2.135 2.181 2.13 2.137 2.071 2.048 2.129 2.067 2.042 1.945 Net change -0.19 a N—k m wuowmthWo< 98 Thickness vs time N to;_ro AOIN 1'3 § 0 Series1 c 2.05 ' 1‘ a :PdY- 13:06511‘ E 2 1 l- 1-95 R2=0.8211 ‘ l 1.9 0 5 10 15 20 25 1 l l Time(days) Figure 44. Relationship between change Thickness under constant load at 25°C and 50% RH(* 2-inch Green Cell® foam) 99 3.3 Moisture Sorption Moisture Sorption lsotherm. Sorption isotherms of the biodegradable starch based foam (Green Cell®) were determined at 20°C, 25°C and 30°C at several relative humidity conditions, by plotting equilibrium moisture content of the product against water activity of the product experimentally and the GAB model. In order to do this, it was necessary to determine the foam moisture content. A Gravimetric method was used to determine foam moisture content . Sorption isotherm at different %RH and 20°C, 25°C and 30°C. Since Green Cell® foam is biodegradable, it absorbs moisture, which affects its packaging performance properties. Moisture sorption isotherms at three temperatures were developed to determine the moisture sensitivity of the product. Gesamtverband der Deutschen versicherungswirtschaft e.v defines the term hygroscopity as the “capacity of a product to react to the moisture content of the air by absorbing or releasing water vapor. Of decisive significance for the absorption or release of water vapor is the water of a product”[27]. Further the sorption isotherm is defined, as “A sorption isotherm is the graphic representation of the sorption behavior of a substance. It represents the relationship between the water content of a product and the relative humidity of the ambient air (equilibrium) at a particular temperature”. 100 Sorption behavior of a hygroscopic product is related to its ability to absorb or release water vapor from air (or into the air) until equilibrium is reached. Sorption isotherms were plotted to determine the moisture sensitivity of the Green Cell® Foam. Initial moisture content (Mi) of the foam was determined to be 1.26%. Moisture sorption isotherms were determined at three different temperatures 20°C; 25°Cand 30°C. The GAB model was then used to obtain the best fit of the data. Quadratic regression analysis was performed by plotting aw/Me vs Me to obtain various model constants. The material was much more hygroscopic at higher temperatures as compared to lower temperature. Green Cell® foam was shown to have a hygroscopic nature. The sorption isotherm profile is a characteristic of the hygroscopic nature of a product. The sorption behavior of a product is dependent on temperature. Highly hygroscopic products exhibit a steep sorption isotherm, while sparingly hygroscopic products exhibit flat sorption isotherms [27]. The hygroscopic nature of a product can be judged by the magnitude of the increase or decrease of a product’s water content as a function of relative humidity or water activity at a certain temperature. Weakly hygroscopic products exhibit no or only a slight change in their water content as a consequence of variations in relative humidity. In strongly hygroscopic products, water content may vary widely [27], which was found to be the case for Green Cell® foam. Types of Sorption isotherm: Generally in the literature three types of sorption isotherm are considered. 1) Sorption isotherm in which the product shows strong hygroscopic nature. As shown‘in Figure 45,this product exhibits a steep rise in product moisture content as a function of %RH. 101 WCZ EST 30"" 25 «.- 20 ~r- lS-- 10 *1- o 1?: sin 2&3 42) sin ti: 'fio an: 9E) idmr""""l #1— Figure 45. Plot between the moisture content (%) and relative humidity RH (%) 2) Sorption isotherm, in which the product exhibits an S-shaped profile, as, shown in Figure 46 Water cnntent Z 35-- 301* 25 ...- 10'“ 5+- : n T Y :::: 1' WW' 010203040506008090100 Figure 46. Plot between the moisture content (%) and relative humidity RH (%) 102 The flat linear portion of this graph represents the most stable form of the product. Above and below this region, harmful changes may occur in the product. [27] 3) Anhydrous product generally exhibits 10w hyrosocopicity, however, once the flow moisture point has been reached, the product rapidly absorbs large amounts of water vapor, its exhibits a deliquesce (hydrous form), as shown in figure 47. Many crystalline products (salt, sugar, potash, tartaric acid) exhibit this behavior. [27]. Equilibrium sorption isotherm provides information about the hydroscopic nature of material. [19] Water content % SS-F 130-1- 25 -- 20-1- 15 w- 10 -‘- 5.1- 0 1'0 2'0 3'0 4'0 5'0 6'0 7'0 8'0 9'0 1 00L 4A A Figure 47. Plot between the moisture content (%) and relative humidity RH (%) Sorption behavior of Green Cell® Foam was found to more closely resemble with type two at 20°C, 25°Cand 30°C as shown Figure No. 48. 49 and 50. Sorption isotherm was determined using a liner method and graphical representation is shown in the following figures 48-50. 103 0.4 0.35 11- — .0 w 1 0.25 ~» , 0.15 ~ 1 .0 o 01 1 T Equlibrlum water content(Me)(g) O N 1 O y = 0.2749x + 0.0208 0 - _- ~ 1 * *- R2 = 0.8549 '+ Me ]—_Linear (Me) 0.00 Figure 48. 0.20 0.40 0.60 0.80 1.00 water activity(Aw) Sorption isotherm of GCF at 20°C Equilibrium moisture content(Me)(g) y = 0.3545x - 0.0117 R2 = 0.811 1+ Me .—_ WMLifnear (Me) Water activity(Aw) Figure 49. Sorption isotherm of GCF at 30°C 104 0.3 0.25 - y = 0.2422x - 0.0011 0.2 . R2 = 0.8918 1] A Lilear (Me) 0.1 1 0.05 Equilbrium moisture content(Me)(g) Water activity Figure 50. Sorption isotherm of GCF at 25°C Since the product did not follow a linear relationship between the aW and Me, the GAB model was selected to represent the sorption isotherm. GAB (01, B, Y) constants were taken from slope of the line for aw/Me vs. aw and calculating T, C, Wm and K to get the calculated GAB value. T, C, Wm and K (GAB constants) were calculated using the following formula. Detailed calculations can be seen in appendix-C, moisture sensitivity of Green Cell® Foam. T fij+4 -ory C r :l: r T2 — 4T)"2 2 w...= 1/13 [ 1- 2/C] K = 1/7 *1/Cw... 105 Calculation of Me (cal) can be achieved using the following expression M = CkAw Wm (l-kAw) (l-kAw+CkAw) Substituting the values into the above equation and solving for Mme, gives a value of Me (cal) at different water activities. The RMS values are calculated using the following formula. RMS = \1[2{(Mexp _ Mcal)/Mexp}2 /N] * 100 Sorption isotherm by GAB Model: GAB model (01, B, y) constants were taken from the slope of the following Graph(figure 51) in order to get the calculated Me (GAB) values at 20°C ) _y =;1_1_.1o1x’_+ 13.55:: - 0.1467 __ R2 :- 0.9892 awlllo N 1 {14 05 DEL (17 QB 09 Water activ lty(aw) Figure 51. Plot of aw/Me and water activity at 20°C 106 Comparison of GAB model (calculated values) and experimental values of Me are shown. Detailed calculations are shown in appendix-C, Moisture sensitivity of Green Cell® Foam. The RMS value was calculated to be 5.00. 0.3 8 0.25W W n, f ,- -0 "6 2 g 0.2 - _ 8 :9} 0.15W- - ,, C s S o 0'1 i 0 Experimental ‘ T g —I—GAB ‘ I» 0.05 W30. - 2-- O E o . o 02 0.4 06 08 1 aw Figure 52. Comparison of Moisture sorption isotherm for Green Cell Foam based on experimental data and GAB model at 20°C [5-a]. To plot the sorption isotherm using the CAB model at 25° C GAB model (01, B, y) constants were taken from the slope of the following Graph (figure 53) to get the calculated Me values. 107 Plot of Aw/M Vs Aw 6 o 5 __ fl _ ._ . o 4 1 _ _ WWW W W W _ E31 -- *4 WWW—WW - ----~y=-1L635x’W*18.702x¢0.1599. -0- 4-.- g a (21* W -___ -_0Rz'°9‘£’ H _ n - _ 11W W _ WWW W -W ,____ _ _ .W W. W 0 . . . . _1 (L 0.1 0.2 0.3 0.4 - 0.5 0.6 0.7 0.8 09 AW Figure 53. Graph between aw/Me and water activity at 20°C The GAB isotherm and experimental values at 25°C is presented in figure 54. “6 9 0.3 O N 0.25«» W- - — _ - . m E O Experimntal . g“ 0.2 ..__ ___ .- -_ m E 3! 0‘ 0.15 W-W- W W- a 8 0 0 0.1 W- WW __ _m 2 M :3 0.05/ ‘ ~ W 40A- 0 2 o . 0 0.2 0.4 0.6 0.8 1 Aw Figure 54. Moisture sorption isotherm of Green Cell® foam at 25°C. 108 Detailed calculations are presented in appendix-C, Moisture sensitivity of Green Cell® Foam. The RMS value was found to be 8.53 [5-a]. To plot the sorption isotherm at 30 C using the CAB model GAB model (OK, 8, y) constants were taken from the slope of the Graph (figure 55) to get the calculated Me values using the GAB model. Plot of Aw/M Vs Aw v = 412295? + 153543! 99123 R2 . 0.9805 AwIM 43.5 0.1 Q.Z___Q.3___0.4 M 0.1 (LL—.93 1.9 Aw Figure 55. Plot of aw/Me and water activity at 30°C Comparison of the GAB predicted isotherm and the experimental isotherm is shown in figure 56. 109 0.45 0.35W , , - o —- Moisture Content(gofH20/g of solid) Figure 56. Comparison of the moisture sorption isotherm (GAB and experimental) of Green Cell® Foam at 30°C [5-a]. Detailed calculations can be seen in appendix-C, Moisture sensitivity of Green Cell® Foam. RMS value was found to be 8.6847. [5-a] Moisture loss or gain Moisture absorbing/desorbing behavior under different humidity conditions at 20° C,25°C and 30°C is shown in the figures 57 and 59. 110 Moisture gain/loss behavior at 20°C followed the same pattern as GCF at 25°C and 30°C but at a slower rate. Fungus was observed on the GCF at 96%RH afier 35 days of storage. Figure 57. Fungus on GCF at 20 C and 96% RH Most significant weight changes were obserevd at 75%, 84% and 96%. At 75%and 84% RH, material expanded during the first week of storage and gained moisture. At higher humidity conditions like 96% RH, material lost its shape and contracted during the first few days of storage but gained moisture. After the first week of storage, the material again started to expand but never regained its shape. After one month of storage, it was observed that mold was growing on the material which was kept at 96% RH. At 25°C the most significant change can be seen at 75% and 84% .At 75%RH, material expanded during the first week of storage study and gained moisture. No significant physical change was observed at 51%, 35% and 23% RH. 111 At 75% and 84% material gained moisture and also expand. This behavior is shown in the following Figures 58 and 59. Sample kept at RH75°/o Fresh sample And 30 C Figure 58. Comparison of fresh sample and material kept at RH75% and 30°C 2% A5 /. Th“. On kink So MM “P“ 6‘4“... l Fresh sample Sample kept at 95% RH and 30C Figure 59. Comparison of fresh sample and material kept at RH 95% and 30°C 112 At higher Relative humidity conditions (89% and 95%) material lost its shape, contracted but gained moisture. Retrogradation may affect Green Cell® foam at higher humidity conditions and may be why it lost its shape and became brittle. At 43% and 54% no significant change was observed during the storage. The material absorbed moisture at 75%, 84%, 89% and 95% RH at 30°C. At 95% RH, the material absorbed the maximum quantity of moisture as compared to 89% RH, 84%RH and 75% RH. At 95% RH, material absorbed 0.844 grams of moisture during 408 hrs of storage [S—a]. At 89%, material absorbed 0.74 grams, at 84% RH 0.32 grams and at 75% RH 0.177grams.At 11% RH the material lost moisture (-0.10 grams). At higher Relative Humidity conditions (89% and 95%) material shrunk but gained moisture. At 43% and 54% no significant changes were observed At 56% RH the material absorbed only 0.0001 grams of moisture and thus it is concluded the ideal relative humidity conditions for Green C ell® Foam. This behavior is shown in the following graph [5-a]. 113 Net weight change at 3°C :35 +11% RH ‘ 2’ +43% RH . 2 56%RH K 3:3 75%RH 1“ 3,2: +84% RH 1 3 _ . a _ +89%RH ‘ g .1 4. 0;} W “1;, gen“.- £4" 5".) .4 . m. :QEflRl-Ll ...J‘IEQV “v.3 WWW “w {wwmwfl‘xdh l Time(hrs) Figure 60. Net Change in weight at 30°C and different humidity conditions. At 11%, 43% and 54%, no significant changes were observed. Detailed calculations can be seen in appendix B— dimensional changes. The most ideal conditions for the material is at 30°C was 56% RH .L, x W, x T change (—0.01 x —0.01 x0.075) inches) respectively. Ideal conditions for Green Cell® Foam is 56% relative humidity. Net moisture gain at 55% RH and 20°C was only 0.01 grams after 35 days of storage, while at 25°C and 51% RH, net moisture gain was only 0.0008 grams after 15 days of storage. This leads to the conclusion that the ideal storage condition for this material is 50-56% RH at 25°C. The product showed the same pattern of absorbing/desorbing behavior under the different temperature conditions of 20° C, 25°C and 30°C as this pattern. 114 3.4 Thermal insulation Package insulating ability (R Value) and bulk density of Green Cell foam. The insulating ability of Green Cell® foam and EPS coolers was determined at two different conditions (25°C, 50% RH and 30°C, 80%RH). Bulk density of one inch thick and two-inch thick Green Cell® foam was calculated. Bulk density Bulk density is defined as the weight per "unit volume of the material [9] .For one-inch thick foam was found to be 3.071bs/ft3and two inch thick foams was found to be 3.35711bs/fi3 [5-a]. Density values were calculated from triplicate measurements and detailed calculations can be seen in appendix D, R-value and density calculations. Traditionally, expanded polystyrene (EPS) has been the sole foam packaging material used for coolers. The bulk density of Green Cell® foam, is much higher than expanded polystyrene foam and other commercial foams. Total weight of the package would increase substantially because of the higher density of the GCF. Bulk densities range from 1.25 pcf to 2.2pcf,density for EPS, PE, ARC EL512, and polyurethane. R—value: “The R-value Rule has been helpful in comparing different brands of the same type of insulating materials” said Betsy de Campos, executive director of EPSMA, “ but as more sophisticated materials and higher technology construction systems are introduced into the building industry we find that R- value of the material does not tell the whole story.”[23] 115 The R- value is based on the mathematical term known as the R- factor. The term R- value was developed to represent the ability of an insulation material to restrict flow. Thermal resistance of a material is its resistance to heat flow and is expressed as the reciprocal of the material’s thermal conductivity. Simply put, the greater the R-Value the better the insulation. [23] Traditionally, expanded polystyrene (EPS) was the sole foam packaging material [12]. Polystyrene foams are considered to have excellent balance between cost and performance for the insulation and packaging fields. Polystyrene also has superior shock absorbing properties. [13] This, therefore; was the basic reason to compare the R- value of Green Cell® coolers with EPS coolers. EPS and Green Cell® coolers were made to have the same dimensions. Identical buckets (same size and same color) were used in the EPS and Green Cell® coolers. To compare the R— value of Green Cell® cooler with the EPS coolers, experiments were performed at the same time, in the same environments with the same equipment and the same amount of ice. The conditions used a) 50%RH and 25°C b) 30°C and 80% RH It was found that the EPS cooler had a 10% higher R- value than GC at 50% RH and 25°C and at the higher temperature and relative humidity the EPS cooler had 20% higher R —value as compared to Green Cell® cooler. This indicates that Green Cell® degraded with increase in humidity. It absorbed moisture, which increased its thermal conductivity and thus lowered it’s R- value. Thermal conductivity of cellular plastic is directly affected by factors like density, cell size, polymer composition and gas phase. [12] Thermal conductivity of cellular plastic and elastomers is defined by the K factor, which is defined by Fourier’s equation for 116 conduction through homogeneous materials. Total K factor (MC Intire and Keddedy, 1948) is separated into components of different modes of heat transfer .As shown in the following equation. K= ks+kg+kr+kc Where k5 = conduction through solid kg = conduction through gas kr = radiation kc = convection in the gas These factors can affect the R-value of cellular plastic foams. As density increases, kr (thermal conductivity due to radiation) decreases but in this case no mode of radiation and convection existed only conduction was available, which is responsible for the R- value. The overall change in k usually decreases with increase in density to a minimum at 2pcf(lbs per cubic feet) [12] and then increases with increasing density of the foam above 2 pcf. Since the R- value is the reciprocal of K factor [12], thus Green Cell® will have a lower R— value than the EPS cooler because of its higher density. (3.3pct). At higher relative humidity conditions Green Cell® shows a greater discrepancy than EPS (about 20%) as the material has a more hygroscopic nature as compared to EPS and picks up moisture at a faster rate. 117 At higher humidity conditions, the carbohydrates in Green Cell® foam can absorb more moisture than EPS, thus causing a decrease in the R-value. Green Cell® polymer composition and cell size at different humidity conditions effect R-values. It is difficult to extrapolate, based on these studies, R-values of Green Cell® foam at other temperatures, because of the direct effect of relative humidity. R-value is not linear with temperature and RH increase. Table 11. R-values of EPS cooler and Green Cell cooler at different conditions [5-a]. Temp. RH Time EPS Green Cell® R-Value °F % hr Unit 77 50 24 14.2019 13.24 fi2*h.r*°F/BTU 77 50 48 12.8250 11.918 fi2*hr*°F/BTU 86 80 26 10.0455 7.803 ft2*hr*°F/BTU * Dimensions of EPS cooler and Green Cell cooler: l 1W l6"‘10”8*9” 8 118 CHAPTER 4 CON SLUSION S Biodegradable packaging materials will find niche markets as long as their properties are comparable to currently used synthetics. Dimensional stability is an important parameter for plastic foams. It represents the ability of a material to retain its original shape and size in varying environmental conditions. Since GCF is a hygroscopic material it was not able to retain its dimensions at high RH and temperature conditions. Cushioning characteristics of Green Cell® Foam are also affected by high temperature, high RH and long storage time. Green Cell® Foam can be used for those products such as electronics which are not moisture sensitive and have fragility level 30-45 G. One-inch foam can be used for rugged appliances when these items are shipped and stored in controlled environments for a short period of time. Thermal insulation properties of Green Cell® Foam showed comparable results with EPS at standard RH and temperature (25 °C, 50% RH) conditions. Green Cell® coolers could be an effective package for pharmaceuticals when these items are shipped and stored in controlled environments for short periods of time. Green Cell® Foam is a hygroscopic material whose properties change substantially at high RH. For high RH applications, and for the packaging of produce and other perishables, this will need to be addressed to create more opportunities for its use as packaging foam. 119 4.2 RECOMMENDATIONS Polymer composition and cell size of Green Cell® at different humidity conditions should be investigated and affect of these factor upon R-values are those points which are recommended for further study. Molecular structure of Green Cell® Foam would be studied in depth to investigate its hydroscopic nature. 120 APPENDIX A CUSHIONING CHARACTERISTICS ' Tables G 1 to G 7 represent the information about the shock characteristics of Green Cell® foam having thickness of 1 inch. Table G1. Shock characteristics Shock characteristics 1" thickness Weight = 12.8|bs Area=64in2 Static pressure=0.2 psi Gate time=3.67 Height =24in Filter = 156 s.no G value time Velocity 1 56.76 17 187.06 2 55.56 17.2 187.6 3 56.29 16.9 186.07 4 57.41 17.5 196.37 5 57.09 17.7 193.69 Ave. 56.622 17.26 190.158 s.dev 0.7241 0.3362 4.5803 Table G2. Shock characteristics Shock characteristics 1" thickness Weight = 12.8|bs Aear=36in2 Static pressure=0.355 psi Gate time=3.67 Height =24in Filter = 156 s.no G value time Velocity 1 59.39 17.3 195.45 2 64.92 16.1 197.76 3 61.28 16.4 196.31 4 65.04 15.8 198.03 5 64.29 15.9 195.96 Ave. 62.984 16.3 195.02 s.dev 2.5249 0.6042 1.1352 121 Table G 3. Shock characteristics Shock characteristics 1" thickness Weight = 51lbs Aear=64in2 Static pressure=0.8 psi Gate time=3.67 Height =24in Filter = 156 .no G value time Velocity 1 79.6 12.9 196.35 2 78.12 12.9 193.67 3 80.93 12.6 194.22 4 84.26 12 193.37 5 81.11 12.4 193.69 Ave. 80.804 12.56 195.02 s.dev 2.2752 0.3782 1 .2078 Table G4. Shock characteristics Shock characteristics 1" thickness Weight = 47|bs Aear=36in2 Static pressure=1.305 psi Gate time=3.67 Height =24in Filter =156 s.no Gvalue time VelocitLl 1 117 10.3 226.42I 122 Table G5. Shock characteristics Shock characteristics 1" thickness Weight = 52|bs Aear=36in2 Static pressure=1.44 Gate time=3.67 Height =24in Filter = 156 6 value 122.1 107. 117.3 115.806 7 Table G 6. Shock characteristics Shock characteristics 1" thickness Weight = 57|bs Aear=36in2 Static pressure=1.58 Gate time=3.67 Height =24in Filter = 156 s.no G value time Velocity 1 114.18 10.6 219.51 2 124.69 9.6 223.1 3 112.62 10.4 219.62 Ave. 117.1633 10.2 220.7433 s.dev 6.5648 0.5292 2.0417 123 Table G7.Shock characteristics Shock characteristics 1" thickness Weight = 62|bs Aear=36in2 Static pressure=1.722 Gate time=3.67 Height =24in Filter = 156 s.no G value time Velocity 1 131.47 9.6 229.4 2 130.92 9.3 228.96 3 130.23 9.5 226.49 Ave. 130.8733 9.4667 228.2833 s.dev 0.6213 0.1528 1.5686 124 ' Tables G 8 to G16 represent the information about the shock characteristics of Green Cell® foam having thickness of 2- inch. Table G8. Shock characteristics Shock characteristics 2" thickness Weight =12.8lbs Area =36in2 Static pressure = 0.355 psi Gate time =3.67 Height = 24in Filter = 156 s.no G value time Velocity l 39.97 22.8 177.25 2 38.58 23 170.57 4 39.22 22.9 172.57 6 39.15 22.1 169.92 7 38.42 22.8 169.86 ave. 39.0680 22.7200 172.0340 st dev. 0.6127 0.3564 3.1158 125 Table G 9. Shock characteristics Shock characteristics 2" thickness Weight = 37lbs Area = 64in2 Static pressure = 0.578 Gate time = 3.67 Height = 24in Filter = 156 s.no G value time Velocity 1 34.61 21.5 164.56 2 38.3 20.7 166.49 3 37.99 20.5 167.81 4 34.1 21.8 165.1 5 31.96 21.9 162.47 Ave. 35.392 21.28 165.286 s.dev 2.7049 Table G 10. Shock characteristics Shock characteristics 2" thickness Weight = 421bs Aear=64in2 Static pressure=0.65625 Gate time=3.67 Height =24in Filter = 156 s o Gvalue time Velocity 34.65 22.5 169.45 31.75 22.9 165.88 31.16 22.9 166.67 34.59 22 170.05 Mauro—M: 31.79 22.9 165.86 Ave. 32.788 22.64 167.582 s.dev 1.6910 126 Table G11. Shock characteristics Shock characteristics 2" thickness Weight = 51.001bs Aear=64in2 Static pressure=0.8125 Gate time=3.67 Height =24in Filter = 156 s.no G value time Velocity l 37.14 21.1 168.34 2 38.23 23 168.26 3 34.54 21.6 175.91 4 29.56 25.7 161.83 Ave. 34.8675 22.85 168.585 s.dev 3.8621 Table G12. Shock characteristics Shock characteristics 2" thickness Weight = 521bs Aear=36in2 Static pressure=1.444 psi Gate time=3.67 Height =24in Filter = 156 s.no G value time Velocity 1 40.03 23.9 174.2 2 40.96 21.8 171.93 3 40.01 21.7 170.31 4 48.65 20.6 189.95 5 40.31 21.8 167.7 Ave. 41.992 21.96 174.818 s.dev 3.7417 1.1971 8.7848 127 Table G 13. Shock characteristics Shock characteristics 2" thickness Weight = 57le Aear=36in2 Static pressure=1.583 psi Gate time=3.67 Height =24in Filter = 156 s.no G value time Velocity 1 36.97 21 158.4 2 36.63 22.3 162.21 3 31.55 22.6 143.42 4 31.7 22.8 142.45 5 31.31 24.1 148.79 Ave. 33.632 22.56 151.054 s.dev 2.8978 1.1104 8.8861 Table G 14. Shock characteristics Shock characteristics 2" thickness Weight = 621bs Aear=36in2 Static pressure=1.722 psi Gate time=3.67 Height =24in Filter = 156 o G value time Velocity 39.57 21.5 164.46 43.13 22.3 178.81 39.75 20.8 163.49 hWNu—Ib 41.15 21.4 174.37 Ave. 40.9 21.5 170.2825 s.dev 1.6459 0.6164 7.5159 128 Table G 15. Shock characteristics Shock characteristics 2" thickness Weight = 63.3le Area=36in2 Static pressure=1.758 psi Gate time=3.67 Height =24in Filter = 156 s.no G value time Velocity 1 37.52 21.8 161.13 Table G16. Shock characteristics Shock characteristics 2" thickness Weight = 12.8|bs Aear=36in2 Static pressure=0.355 Gate time=3.67 Height =24in Filter = 156 129 . Table G17 represents the shock characteristic information before storing at different humidity conditions and 30°C and table G 18 represents shock characteristic information after the storage study at different humidity conditions and 30°C. Table G17. Shock characteristic information before storing at different humidity conditions and 30°C. Date: 10/21/2003 s.no G value time Velocity Wt. of sample G's ms in/sec g 1 39.97 22.8 177.25 51.62 2 38.58 23 170.57 52.65 3 32.18 25.2 158.19 54.58 4 39.22 22.9 172.57 51.86 5 32.9 25.8 164.47 56.34 6 39.15 22.1 169.92 51.51 38.42 22.8 169.86 52.38 Ave. 37.203 23.51429 168.976 s.dev 3.2311 1.3981 6.0859 Table G18. Shock characteristic information after the storage study at different humidity conditions and 30°C. s.no RH % G value time velocity wt. Of sample % G's ms in/sec g 1 11 51.84 17 182.63 58.68 2 43 45.21 18.1 174.4 52.64 3 54 38.29 21 171.59 54.7 4 75 36.53 22.6 169.08 53.96 5 86 37.25 18.8 153.64 62.03 6 89 50.63 16.4 163.43 60.59 7 97 76.77 12.4 184.1 67.31 130 I Table G19 (a, b and c). Shows the comparison of shock characteristics of Green Cell® foam before the storage study and after the storage study at different relative humidity (%RH) conditions and 30°C.(Table G19-a) Table G19 (a) 10/21/03 12/23/03 10/21/03 12/23/03 Aw s.no RH G value G value wt. wt. net wt. gain % (8) (8) (g) 1 11 39.97 51.84 51.62 52.68 1.06 2 43 38.58 45.21 52.65 52.64 -0.01 3 54 32.18 38.29 54.58 54.7 0.12 4 75 39.22 36.53 51.86 53.96 2.1 5 86 32.9 37.25 56.34 62.03 5.69 6 89 39.15 50.63 51.51 60.59 9.08 7 97 38.42 76.77 52.38 67.31 14.93 (Table G19-b) Date 10/21/2003 12/23/2003 10/21/2003 12/23/2003 s.no RH time time velocity velocity % (ms) (ms) (in/sec) (in/sec) 1 11 22.8 17 177.25 182.63 2 43 23 18.1 170.57 174.4 3 54 25.2 21 158.19 171.59 4 75 22.9 22.6 172.57 169.08 5 86 25.8 18.8 164.47 153.64 6 89 22.1 16.4 169.92 163.43 7 97 22.8 12.4 169.86 184.1 Table G19. Comparison of G values of Green Cell® foam at different relative humidities and time (days) Table 19-c) Time RHl 1 1% RH 45% RH 56% RH 77% RH 8400% RH90% RH 96%| 10/21/03 39.97 38.58 32.18 39.22 32.9 39.15 38.42 I 12/23/003 51.84 45.21 38.29 36.53 37.25 50.63 76.77 I 131 time (days) Graph between G values and time 90 . 80 ~ —, 1 o RH11°/o ‘ a 70 ’ J I RH 45% 5 £3 60 ” ‘ 7 '7 ‘ RH 56% l 3 50 h . ’1 1 RH 77°/ 1? 7:; 40 7 ’9 x ’ l 00 ll > 30 1, x f , .. :1: RH 8400/...g (D 20 WW -W -_ W - W W W WWWWWWW .W W WWWW .4 O RH90% ‘ 10 W W + RH 96% l 0 . 10/6/200 10/26/20 11/15/20 12/5/200 12/25/20 1/14/200 1 3 03 03 3 O3 4 Figure G1. Graph between G value and Time (days) Table G 20. Comparison of G values of Green Cell® foam at different relative humidities with respect to time lRH % 10/21/2003 12/23/2003 1 1 39.97 51 .84 45 38.58 45.21 56 32.18 38.29 77 39.22 36.53 84 32.9 37.25 90 39.15 50.63 96 38.42 76.77 132 copmarison of G values 70710/2—172-063 . 12/23/2003. G values Relative Humidity(RH°/n) Figure G 2. Graph between G values and Relative Humidity conditions (RH%) Shock characteristics and time effect Table G 21. Shock characteristics of Green Cell® foam Shock characteristics 2" thickness Weight = 51.001bs Aear=64in2 Static pressure=0.8125 Gate time=3.67 Height =24in Filter = 156 G value 37. 4 34.54 29.56 133 Table G 22. Shock characteristics of Green cell foam Shock characteristics 2" thickness Weight = 51.001bs Aear=64in2 Static pressure=0.8125 Gate time=3.67 Height =24in Filter = 156 Time : Sept.19,2003 s.no Gvalue time Velocity Condition l 22.05 30.1 130.95 Platen donot bounces back 2 24.28 28.2 130.67 Platen donot bounces back 24.28 28.5 134.34 Platen donot bounces back 24.88 27.6 133.59 Platen donot bounces back (II-bu) 25.6 27 137.1 Platen donot bounces back Ave. 24.218 28.28 133.33 Platendonotbouncesback s.dev 1.3282 laten donot bounces back Table G 23. Shock characteristics of Green cell foam Time oct. 21,2003 2nd set of material fresh samples Weight = 51.001bs Aear=64in2 Static pressure=0.8125 Gate time=3.67 Height =24in Filter = 156 s.no G value time Velocity ms in/sec 1 34.28 21.1 166.34 2 37.32 23.2 168.34 3 34.54 21.6 173.91 4 37.14 24.7 161.83 5 35.38 23.02 169.29 ' Ave. 36.095 22.724 167.942 s.dev 1.3567 1.424739 4.4021438 134 Table G24. Shock characteristics of Green cell foam Shock characteristics 1" thickness Weight = 511bs Aear=64in2 Static pressure=0.8 psi Gate time=3.67 Height =24in Filter = 156 Time : July 15, 2003 s.no G value time(ms) Velocity(in/sec) 1 79.6 12.9 196.35 2 78.12 12.9 193.67 3 80.93 12.6 194.22 4 84.26 12 193.37 5 81.11 12.4 193.69 Ave. 80.804 12.56 195.02 s.dev 2.2752 0.3782 1.2078 Table G 25. Shock characteristics of Green cell foam Shock characteristics 1" thickness Weight = 511bs Aear=64in2 Static pressure=0.8 psi Gate time=3.67 Height =24in Filter = 156 Time : Sept 19,2003 s.no G value time(ms) Velocity(in/sec) 1 55.84 14.8 173.52 2 51.41 15.7 166.83 3 47.59 16.6 167.4 4 51.89 15.2 165.76 Ave 51.683 15.575 168.3775 s.dev 3.3740 0.7762 3.4951 135 Another attempt Weight = 511bs Aear=64in2 Static pressure=0.8 psi Gate time=3.67 Height =24in Table G26. Shock characteristics of Green cell foam Filter = 156 Time sept.20,2003 s.no G value time(ms) Velocity(in/sec) l 48.24 16.6 163.12 2 51.39 15.6 167.73 3 52.08 15.2 168.48 4 49.65 16.5 168.78 Ave. 50.34 15.975 167.0275 s.dev 1.7336 0.6850 2.6422 Table G27. Shock characteristics of Green cell foam Shock characteristics 1" thickness Weight = 511bs Aear=64in2 Static pressure=0.8 psi Gate time=3.67 Height =24in Filter = 156 Oct.2l,2003 s.no G value time Velocity 1 79.6 12.9 196.35 2 78.12 12.9 193.67 3 80.93 12.6 194.22 4 84.26 12 193.37 5 81.11 12.4 193.69 Ave. 80.804 12.56 195.02 s.dev 2.2752 0.3782 1.2078 136 Figure G 3. Comparison of Green Cell® foam material kept at 50% RH ,25°C and 11% RH ,30°C.(Front view) Material kept at 1 Material kept at 30C 25C and 50%RH and 11% R11 1 Figure G 4. Comparison of Green Cell® foam material kept at 50% RH, 25°C and 1 1% RH, 30°C.(Side view) 137 Figure G 5. Comparison of Green Cell® foam material kept at 50% RH , 25°C and 43% RH ,30°C.(Front view) Material kept at Material kept at 25C and 50% RH 30C and 43% RH Figure G6. Comparison of Green Cell foam material kept at 50% RH, 25C and 43% RH ,30C.(Side view) 138 Material kept at Material kept at 25C and 50% RH 30C and 43% Figure G 7. Comparison of Green Cell foam material kept at 50% RH, 25C and 43% RH ,30C.(Front view) Material kept at Material kept at 30C 25C and 50% RH and 54% RH Figure G 8. Comparison of Green Cell foam material kept at 50% RH, 25C and 43% RH, 30C.(Side view) 139 APPENDIX B DIMENSIONAL CHANGES AND MOISTURE GAIN/LOSS Dimensional Changes and Moisture gain/loss with respect to time at 11% RH and 30°C. Table D 1. Dimensional change data of sample no. “1” S.No.1 Date Time Length Width Thickness Weight hrs (L) in (W) in (T) in (wt) g 10/22/2003 0 2.1105 2.019 1.1785 4.1529 10/23/2003 24 2.077 2.0045 1.166 4.016 10/24/2003 48 2.1075 1.978 1.1585 4.0182 25-Oct 72 2.109 2.013 1.1785 4.0091 10/27/2003 96 2.0915 2.03 1.1935 4.0378 10/28/2003 120 2.099 2.016 1.19 4.0094 10/29/2003 144 2.122 2.014 1.197 4.0195 11/31/2003 192 2.1025 1.994 1.187 4.0605 1 1/2/2003 240 2.107 2.005 1.2095 4.0715 11/5/2003 312 2.0755 1.996 1.2 4.08 11/7/2003 360 2.083 2.007 1.207 4.0728 11/9/2003 408 2.057 1.987 1.19 4.053 Ave. 2.0951 2.0053 1.1880 4.0501 Table D 2. Dimensional change data of sample no. “l-A” S.No l-A Date time Length Width Thickness Weight hrs (L) in (W) in (T) in (wt) g 10/22/2003 0 2.1025 2.097 1.2865 4.4403 . 10/23/2003 24 2.0865 2.062 1.2508 4.291 10/24/2003 48 2.093 2.112 1.2985 4.2882 25-Oct 72 2.1025 2.128 1.323 4.2842 10/27/2003 96 2.092 2.113 1.3325 4.2978 10/28/2003 120 2.0975 2.1155 1.3235 4.2802 10/29/2003 144 2.1002 2.0915 1.3585 4.2915 11/31/2003 192 2.0985 2.0902 1.334 4.3047 11/2/2003 240 2.114 2.122 1.3645 4.3478 11/5/2003 312 2.1085 2.0995 1.3545 4.3576 11/7/2003 360 2.105 2.0865 1.346 4.3493 11/9/2003 408 2.0915 2.082 1.338 4.3273 Ave. 2.0993 2.0999 1.3259 4.3217 140 Table D 3. Averaged Dimensional Changes (thickness, length and width) data Time Length st.dev Length Width Width st.dev. 1" Net Wt. st.dev. (hrs) (in) net change in net change Thickness Change(g) (in) ' (in) (in) (in) 0 2.0834 0.0269 0.0000 1.9474 0.0000 0.1317 1.2325 0.0000 0.0764 24 2.0505 0.0364 -0.0329 1.9210 -0.0264 0.1319 1.2084 -0.0241 0.0600 48 2.0543 0.0553 -0.0292 2.0001 0.0527 0.1257 1.2285 0.0040 0.0990 72 2.0634 0.0493 0.0200 2.0078 0.0604 0.1231 1.2508 0.0183 0.1022 96 2.0571 0.0413 -0.0263 2.0164 0.0690 0.1067 1.2630 0.0305 0.0983 120 2.0677 0.0384 -0.0158 2.0128 0.0654 0.1040 1.2568 0.0242 0.0944 144 2.0775 0.0417 -0.0060 2.0036 0.0562 0.1012 1.2778 0.0453 0.1142 192 2.0660 0.0402 -0.0174 1.9932 0.0458 0.1120 1.2605 0.0280 0.1039 240 2.0770 0.0392 -0.0064 2.0161 0.0687 0.1189 1.2870 0.0545 0.1096 312 2.0630 0.0368 0.0204 2.0020 0.0546 0.1172 1.2773 0.0448 0.1092 360 2.0561 0.0450 -0.0273 1.9960 0.0486 0.1135 1.2765 0.0440 0.0983 408 2.0410 0.0413 0.0424 1.9863 0.0389 0.1132 1.2640 0.0315 0.1047 Ave. 2.0631 0.0410 1.9919 0.1166 1.2569 0.0975 Dimensional Changes at 11% RH and 30C 0.0800 .3 0.0600 WW. g» 0.0400 +Length net change 2 (in) 1 o 0-0200 l '—l—Width net change To in : 0.0000 ‘ i ( ) l .3 6 0 Thickness Change 5 -0.0200 5“ (in) E a -0.0400 -0.0600 W Time (hrs) Figure Dl-a. Dimensional changes at 11% RH and 30°C. 141 wt. change at 11%RH at 30 C 0 t . 1 1 ¥ 1 00 200 300 400 5&0 -0.1 W W W W W W + "- . 1 -0.15 — W ,. 1,, ave ‘ T"..Z_'a.v§;. . Change(g) wt 95 N 1 -0.25 -. W WWWWW W -0.3 Time(hrs) l ,3 - 5 L, Figure Dl-b. Weight changes at 11% RH and 30°C. 142 Dimensional Changes and Moisture gain/loss with respect to time at 43% RH and 30°C. Table D 4. Dimensional Changes data at 43% and 30°C. Length ate 10/22/03 10/23/03 10/24/03 25-Oct 10/27/03 10/28/03 s.no. hrs 0 24 8 72 96 120 43-B 2.096 2.108 2.107 2.098 2.108 2.1045 43-B-1 1.936 1.964 1.9965 1.9805 1.994 1.983 Ave. 2.016 2.036 2.05175 2.03925 2.051 2.04375 st.dev .1131 .1018 0.0781 0.0831 0.0806 0.0859 Width ate 10/22/03 10/23/03 10/24/03 25-Oct 10/27/03 10/28/03 Is.no hrs 0 24 48 72 96 120 43-B 1.918 1.9435 1.9445 1.9535 1.936 1.964 43-B-1 2.0735 2.049 2.094 2.081 2.077 2.0615 Ave. 1.99575 1.9435 2.01925 2.01725 2.0065 2.01275 st.dev 0.1 100 .0746 .1057 .0902 0.0997 .0689 Thickness Date 10/22/03 10/23/03 10/24/03 25-Oct 10/27/03 10/28/03 .no hrs 0 24 48 72 96 120 43-B 1.258 1.2625 1.275 1.2765 1.287 1.2925 3-B-l 1.187 1.2155 1.212 1.2145 1.219 1.2275 Ave. 1.2225 1.239 1.2435 1.2455 1.253 1.26 t.dev 0.0502 .0332 0.0445 .043 8 .0481 0.0460 wt. change I Date 10/22/03 10/23/03 10/24/03 5-Oct 10/27/03 10/28/03 |s.no. hrs 0 24 48 72 96 120 43-B 4.1342 4.0945 4.0908 4.0915 4.0865 4.0835 43-B-1 3.9382 3.9011 3.8989 3.8974 3.8951 3.8919 Ave. 4.0362 3.9978 3.99485 3.99445 8.9908 3.9877 8t.dev 0.1386 0.1368 0.1357 .1372 .1353 .1355 143 (continued from Table D4) Length Date 10/29/2003 11/31/200311/2/2003 11/5/200311/7/2003 11/9/2003 S.no. hrs 144 192 240 312 360 408 43-B 2.0955 2.096 2.097 2.09 2.0735 2.0795 43-B-1 1.9735 1.982 1.983 1.987 1.9615 1.971 Ave. 2.0345 2.039 2.04 2.0385 2.0175 2.02525 st.dev 0.08626703 0.0806102 0.080610170072832 0.07919596 0.07672109 Width Date 10/29/2003 11/31/200311/2/2003 11/5/200311/7/2003 11/9/2003 1s.no hrs 144 192 240 312 360 408 43-B 1.9475 1.9535 1.9555 1.935 1.9205 1.944 43-B-1 2.0635 2.095 2.093 2.0445 2.016 2.0395 Ave. 2.0055 2.02425 2.02425 1.98975 1.96825 1.99175 st.dev 0.0820 .1001 0.0972 0.0774 0.0675 .0675 Thickness I Date 10/29/2003 11/31/200311/2/2003 11/5/200311/7/2003 11/9/2003 .no hrs 144 192 240 312 360 408 43-B 1.291 1.2865 1.2873 1.28 1.267 1.2805 43-B-1 1.2165 1.226 1.229 1.2115 1.1955 1.295 Ave. - 1.25375 1.25625 1.25815 1.24575 1.23125 1.28775 [st.dev .0527 0.0428 0.0412 .0484 0.0506 .0103 wt. change Date 10/29/2003 11/31/200311/2/2003 11/5/200311/7/2003 11/9/2003 Is.no. hrs 144 192 240 312 360 408 43-B 4.0834 4.0843 4.0848 4.083 4.0825 4.0815 43-B-1 3.8924 3.8953 3.8952 3.8915 3.8908 3.8905 Ave. 3.9879 3.9898 3.99 3.98725 3.98665 3.986 jst.dev 0.1351 .1336 .1341 0.1354 0.1356 0.1351 144 Table D 5-D8: Net Dimensional changes and weight loss/gain at 43% RH and 30°C. Length Table D5: Change in length with respect to time Net change Date hrs Length st.dev Length 10/22/2003 0 2.0160 0.1 131 0 10/23/2003 24 2.0360 0.1018 0.020 10/24/2003 48 2.0518 0.0781 0.036 25-Oct 72 2.0393 0.0831 0.023 10/27/2003 96 2.0510 0.0806 0.035 10/28/2003 120 2.0438 0.0859 0.028 10/29/2003 144 2.0345 0.0863 0.019 1 1/31/2003 192 2.0390 0.0806 0.023 1 1/2/2003 240 2.0400 0.0806 0.024 1 1/5/2003 312 2.0385 0.0728 0.023 1 1/7/2003 360 2.0175 0.0792 0.002 1 1/9/2003 408 2.0253 0.0767 0.009 Width Table D 6. Change in Width with respect to time Net change Date hrs Width st.dev Width 10/22/2003 0 1.9958 0.1100 0 10/23/2003 24 1.9435 0.0746 -0.0523 10/24/2003 48 2.0193 0.1057 0.0235 25-Oct 72 2.0173 0.0902 0.0214 10/27/2003 96 2.0065 0.0997 0.0107 10/28/2003 120 2.0128 0.0689 0.0170 10/29/2003 144 2.0055 0.0820 0.0097 11/31/2003 192 2.0243 0.1001 0.0285 1 1/2/2003 240 2.0243 0.0972 0.0284 1 1/5/2003 312 1.9898 0.0774 -0.0060 1 1/7/2003 360 1.9683 0.0675 -0.0276 11/9/2003 408 1.9918 0.0675 -0.0041 145 Thickness TableD7. Change in Thickness with respect to time Net change Date hrs Thickness st.dev Thickness 10/22/2003 0 1.2225 0.0502 0 10/23/2003 24 1.2390 0.0332 0.0165 10/24/2003 48 1.2435 0.0445 0.0210 25-Oct 72 1.2455 0.0438 0.0230 10/27/2003 96 1.2530 0.0481 0.0305 10/28/2003 120 1.2600 0.0460 0.0375 10/29/2003 144 1.2538 0.0527 0.0313 1 1/31/2003 192 1.2563 0.0428 0.0338 11/2/2003 240 1.2582 0.0412 0.0357 1 1/5/2003 312 1.2458 0.0484 0.0233 1 1/7/2003 360 1.2313 0.0506 0.0088 11/9/2003 408 1.2878 0.0103 0.0653 Weight Change TableD 8. Moisture gain/loss with respect to time Net change Date hrs wt.(g) st.dev. wt. Change 10/22/2003 0 4.0362 0.1386 0.0000 10/23/2003 24 3.9978 0.1368 -0.03 84 10/24/2003 48 3.9949 0.1357 -0.0414 25-Oct 72 3.9945 0.1372 -0.0418 10/27/2003 96 3.9908 0.1353 -0.0454 10/28/2003 120 3.9877 0.1355 -0.0485 10/29/2003 144 3.9879 0.1351 -0.0483 11/31/2003 192 3.9898 0.1336 -0.0464 1 1/2/2003 240 3.9900 0.1341 -0.0462 11/5/2003 312 3.9873 0.1354 -0.0489 11/7/2003 360 3.9867 0.1356 -0.0496 11/9/2003 408 3.9860 0.1351 -0.0502 146 Dimensional changes at 43% RH and 3°C 0.08 0.06 l E g 0.04 g —W—W: E 0.02 +Length ‘ 2 +Width ‘ g 0 Thickness “ l 5 .002 E n -o.o4 -0.06 l Time(hrs) Figure D 2. Dimensional changes at 43% RH and 30°C. Net Weight Change 0.0000 . . . 100 200 300 400 5130 ’3 0.01001 WW WW W W. Ti 2' 0.0200 .2 ‘5 '7: -0.0400 - 3 0.0500 1 -0.0600 Time(hrs) Figure D 3. Moisture gain/loss at 43% RH and 30°C. 147 Dimensional Changes and Moisture gain/loss with respect to time at 56% RH and 30°C. Table D 9. Dimensional Changes data at 56% and 30°C. Length Date 10/22/2003 10/23/2003 10/24/2003 25—Oct 10/27/2003 10/28/2003 S.no. Time(hrs) 0 24 48 72 96 120 56—B 1.964 1.966 1.985 1.973 1.969 2.0025 56—B-1 2.03 2.048 2.0305 2.0085 1.986 2.04 Ave. 1.997 2.007 2.00775 1.9907 1.9775 2.02125 st.dev 0.0467 0.0580 0.0322 0.0251 0.0120 0.0265 Width Date 10/22/2003 10/23/2003 10/24/2003 25-Oct 10/2 7/2003 10/2 8/2003 s.no Time(hrs 0 24 48 72 96 120 56-B 2.085 2.0888 2.09 2.0805 2.096 2.1005 56-B-l 2.0185 2.045 2.0485 2.0595 2.061 2.0885 Ave. 2.05175 2.0888 2.06925 2.07 2.0785 2.0945 st.dev 0.0470 0.0310 0.0293 0.0148 0.0247 0.0085 Thickne 55 Date 10/22/2003 10/23/2003 10/24/2003 25-Oct 10/27/2003 10/28/2003 s.no Time(hrs) 0 24 48 72 96 120 56-B 1.2455 1.2835 1.2615 1.2945 1.317 1.321 56-B-1 1.229 1.255 1.2635 1.275 1.2845 1.285 Ave. 1.23725 1.26925 1.2625 1.28475 1.30075 1.303 st.dev 0.01 17 0.0202 0.0014 0.0138 0.0230 0.0255 wt. change Date 10/22/2003 10/23/2003 10/24/2003 25-Oct 10/27/2003 10/28/2003 s.no. Time(hrs) 0 24 48 72 96 120 56-B 3.5927 3.5958 3.5987 3.5975 3.5956 3.6 56-B-1 3.9728 3.9752 3.9797 3.9776 3.9758 3.9791 Ave. 3.78275 3.7855 3.7892 3.78755 3.7857 3.78955 st.dev 0.2688 0.2683 0.2694 0.2688 0.2688 0.2681 148 (Continued from table D9) Length Date 10/29/2003 1 1/31/2003 1 1/2/2003 1 1/5/2003 1 1/7/2003 1 1/9/2003 S.no. Time(hrs) 144 l 92 240 3 12 360 408 56-B 1.989 1.99 1.9855 1.966 1.9625 1.9665 56-B-1 2.006 2.0335 2.018 1.997 1.9955 2 Ave. 1.9975 2.01 175 2.00175 1.9815 1.979 1.98325 st.dev 0.0120 0.0308 0.0230 0.0219 0.0233 0.0237 Width Date 10/29/2003 1 1/31/2003 11/2/2003 1 1/5/2003 1 1/7/2003 1 1/9/2003 s.no Time(hrs) 144 192 240 3 12 360 408 56-B 2.0815 2.0875 2.082 2.071 2.044 2.064 56-B-l 2.041 2.0565 2.056 2.034 1.999 2.0195 Ave. 2.06125 2.072 2.069 2.0525 2.0215 2.04175 st.dev 0.0286 0.0219 0.0184 0.0262 0.0318 0.0315 Thickness Date 10/29/2003 1 1/31/2003 11/2/2003 1 1/5/2003 1 1/7/2003 11/9/2003 5 -no Time(hrs) 144 1 92 240 3 12 360 408 561-3 1.3175 1.3625 1.3515 1.321 1.3105 1.359 56—B-1 1.271 1.2745 1.2665 1.2645 1.2465 1.266 [1 Ave. 1.29425 1.3185 1.309 1.29275 1.2785 1.3125 ll st.dev 0.0329 0.0622 0.0601 0.0400 0.0453 0.0658 wt. change Date 10/29/2003 1 1/31/2003 11/2/2003 1 1/5/2003 1 1/7/2003 1 1/9/2003 s.no. Time(hrs) 144 192 240 3 12 360 408 56-B 3.5958 3.602 3.5987 3.5975 3.594 3.5923 56-B-1 3.9756 3.9833 3.9772 3.9748 3.9741 3.9735 Ave. 3.7857 3.79265 3.78795 3.78615 3.78405 3.7829 st.dev 0.2686 0.2696 0.2676 0.2668 0.2688 0.2695 149 Table D10: Change in Length with respect to time Time Length st.dev Net change Date (hrs) (in) Length 10/22/2003 0 1.9970 0.0467 0 10/23/2003 24 2.0070 0.0580 0.0100 10/24/2003 48 2.0078 0.0322 0.0108 25-Oct 72 1.9908 0.0251 -0.0062 10/27/2003 96 1.9775 0.0120 -0.0195 10/28/2003 120 2.0213 0.0265 0.0243 10/29/2003 144 1.9975 0.0120 0.0005 11/31/2003 192 2.0118 0.0308 0.0148 11/2/2003 240 2.0018 0.0230 0.0047 11/5/2003 312 1.9815 0.0219 -0.0155 1 1/7/2003 360 1.9790 0.0233 -0.0180 1 1/9/2003 408 1.9833 0.0237 -0.0138 Table D11. Change in Width with respect to time Time Width Net change Date (hrs) (in) st.dev Width 10/22/2003 0 2.0518 0.0470 0 10/23/2003 24 2.0888 0.0310 0.0370 10/24/2003 48 2.0693 0.0293 0.0175 25-Oct 72 2.0700 0.0148 0.0182 10/27/2003 96 2.0785 0.0247 0.0267 10/28/2003 120 2.0945 0.0085 0.0427 10/29/2003 144 2.0613 0.0286 0.0094 1 1/31/2003 192 2.0720 0.0219 0.0202 1 1/2/2003 240 2.0690 0.0184 0.0172 11/5/2003 312 2.0525 0.0262 0.0007 11/7/2003 360 2.0215 0.0318 -0.0303 11/9/2003 408 2.0418 0.0315 -0.0101 150 Table D12. Change in Thickness with respect to time Time Net change Date (hrs) Thickness st.dev Thickness 10/22/2003 0 1.2373 0.01 17 0 10/23/2003 24 1.2693 0.0202 0.0320 10/24/2003 48 1.2625 0.0014 0.0253 25-Oct 72 1.2848 0.0138 0.0475 10/27/2003 96 1.3008 0.0230 0.0635 10/28/2003 120 1.3030 0.0255 0.0658 10/29/2003 144 1.2943 0.0329 0.0570 11/31/2003 192 1.3185 0.0622 0.0813 1 1/2/2003 240 1.3090 0.0601 0.0718 11/5/2003 312 1.2928 0.0400 0.0555 1 1/7/2003 360 1.2785 0.0453 0.0413 11/9/2003 408 1.3125 0.0658 0.0753 Table D13. Moisture gain/loss change with respect to time Time Weight change Net wt. Date firs) (g) st.dev Change(g) 10/22/2003 0 3.7828 0.2688 0 10/23/2003 24 3.7855 0.2683 0.0027 10/24/2003 48 3.7892 0.2694 0.0064 25-Oct 72 3.7876 0.2688 0.0048 10/27/2003 96 3.7857 0.2688 0.0029 10/28/2003 120 3.7896 0.2681 0.0068 10/29/2003 144 3.7857 0.2686 0.0029 1 1/31/2003 192 3.7927 0.2696 0.0099 1 1/2/2003 240 3.7880 0.2676 0.0051 11/5/2003 312 3.7862 0.2668 0.0034 1 1/7/2003 360 3.7841 0.2688 0.0012 1 1/9/2003 408 3.7829 0.2695 0.0001 151 Dimensional changes at 56% RH and 30°C 0.1000 _ 0.0800-1W” W W WW WW W WW W4 0.0600 ’ 0.0400 1; __ fit; WWW W— W — WWW« 0.0200 « l y \ 0.0000 ' T v . \Ta W_ {10200 ,, "30“ 2Q_ 711193,,400 500 1 .7— 7 T 1 -0.0400 * + Length —I— Width -, chknese- Dlmenslonal changesfln) Time(hrs) Figure D 4. Dimensional changes at 56% RH and 30°C. Net weight Change at 56% RH and 30°C 0.012 0.01 0.008 1 0.006 I + net wt. Change(g) ‘5 0.004 0.002 Net change In weight (g) 0 100 200 300 400 500 Time (hrs) Figure D5 . Moisture gain/loss at 56% RH and 30°C. 152 Dimensional Changes and Moisture gain/loss with respect to time at 75% RH and 30°C. Table D14. Dimensional Changes data at 75% and 30°C. Length Date 10/22/03 10/23/2003 10/24/2003 10/25/2003 10/27/2003 10/28/03 S.no. hrs 0 24 48 72 96 120 75—B 1.968 1.975 1.998 1.966 1.998 1.983 75-B-1 2.043 2.023 2.0245 2.0245 2.028 2.0195 Ave. 2.0055 1.999 2.01125 1.99525 2.013 2.00125 St.dev. St.dev. 0.0530 0.0339 0.0187 0.0414 0.0212 0.0258 Width Date 10/22/2003 10/23/2003 10/24/2003 25-Oct 10/27/2003 10/28/2003 hrs 0 24 48 72 96 120 s.no 75-B 2.0795 2.11 2.1259 2.107 2.1235 2.115 75-B-1 2.048 2.12 2.1281 2.125 2.1395 2.108 Ave. 2.06375 2.11 2.127 2.116 2.1315 2.1115 St.dev. 0.0223 0.0071 0.0016 0.0127 0.0113 0.0049 Thickne ss 10/22/2003 10/23/2003 10/24/2003 25-Oct 10/27/2003 10/28/2003 hrs 0 24 48 72 96 120 s.no 75-B 1.318 1.5615 1.5856 1.6215 1.6585 1.6625 75-B-1 1.249 1.4275 1.48 1.482 1.515 1.5285 Ave. 1.2835 1.4945 1.5328 1.55175 1.58675 1.5955 St.dev. 0.0488 0.0948 0.0747 0.0986 0.1015 0.0948 Weight chan e F 10/22/2003 10/23/2003 10/24/2003 25-Oct 10/2 7/2003 10/28/2003 lliwt. change hrs 0 24 48 72 96 120 s.no. 75-B 4.0916 4.2395 4.2406 4.2558 4.2714 4.2595 75-B-1 4.1859 4.3341 4.346 4.349 4.3638 4.3521 Ave. 4.13875 4.2868 4.2933 4.3024 4.3176 4.3058 St. de v 0.0667 0.0669 0.0745 0.0659 0.0653 0.0655 153 (Continued from table D14) Length Date 10/29/2003 11/31/2003 11/2/2003 11/5/2003 11/7/2003 11/9/2003 S.no. hrs 144 192 240 312 360 408 7513 1.9715 1.971 1.963 1.964 1.96 1.9595 75-B-l 2.018 2.0105 2.0015 2.005 1.996 1.9965 Ave. 1.99475 1.99075 1.98225 1.9845 1.978 1.978 St.dev St.dev. 0.0329 0.0279 0.0272 0.0290 0.0255 0.0262 Width Date 10/29/2003 11/31/2003 11/2/2003 11/5/2003 11/7/2003 11/9/2003 hrs 144 192 240 3 12 360 408 7513 2.1125 2.1795 2.1115 2.103 2.1105 2.0895 75-B-1 2.08 2.142 2.109 2.0975 2.0775 2.0795 Ave. 2.09625 2.16075 2.11025 2.10025 2.094 2.0845 St.dev 0.0230 0.0265 0.0018 0.0039 0.0233 0.0071 Thickness Date 10/29/2003 11/31/2003 11/2/2003 11/5/2003 11/7/2003 11/9/2003 I hrs 144 192 240 312 360 408 II 7513 1.6815 1.705 1.687 1.6985 1.6695 1.6725 [1 758.1 1.531 1.535 1.5485 1.5845 1.505 1.5585 1 Ave. 1.60625 1.62 1.61775 1.6415 1.58725 1.6155 1 St.dev 0.1064 0.1202 0.0979 0.0806 0.1163 0.0806 Weight change ‘wt. change Date 10/29/2003 11/31/2003 11/2/2003 11/5/2003 11/7/2003 11/9/2003 s.no. hrs 144 192 240 312 360 408 75.8 4.2696 4.277 4.2716 4.2758 4.2686 4.268 75-B-1 4.3575 4.3717 4.3681 4.3702 4.3642 4.3644 Ave. 4.31355 4.32435 4.31985 4.323 4.3164 4.3162 St.dev 0.0622 0.0670 0.0682 0.0668 0.0676 0.0682 154 Table D15. Change in Length with respect to time Time Length (in) St.dev. Net change hrs Length (in) 0 2.0055 0.0530 0.0000 24 1.9990 0.0339 —0.0065 48 2.01 13 0.0187 0.0057 72 1.9953 0.0414 -0.0103 96 2.0130 0.0212 0.0075 120 2.0013 0.0258 -0.0042 144 1.9948 0.0329 -0.0108 192 1.9908 0.0279 -0.0148 240 1.9823 0.0272 -0.0233 312 1.9845 0.0290 -0.0210 360 1.9780 0.0255 -0.0275 408 1.9780 0.0262 -0.0275 Table 16: Change in Width with respect to time Time Width St.dev. et change hrs (Width)(in) 0 2.0638 0.0223 0.0000 24 2.1 100 0.0071 0.0462 48 2.1270 0.0016 0.0632 72 2.1160 0.0127 0.0522 96 2.1315 0.0113 0.0677 120 2.1 1 15 0.0049 0.0478 144 2.0963 0.0230 0.0325 192 2.1608 0.0265 0.0970 240 2.1103 0.0018 0.0465 312 2.1003 0.0039 0.0365 360 2.0940 0.0233 0.0303 408 2.0845 0.0071 0.0208 155 Table D17. Change in Thickness with respect to time Time Thickness St.dev. Net change hrs (in) (in) thicknessQn)i 0 1.2835 0.0488 0.0000 24 1.4945 0.0948 0.2110 48 1.5328 0.0747 0.2493 72 1.5518 0.0986 0.2683 96 1.5868 0.1015 0.3033 120 1.5955 0.0948 0.3120 144 1.6063 0.1064 0.3228 192 1.6200 0.1202 0.3365 240 1.6178 0.0979 0.3343 312 1.6415 0.0806 0.3580 360 1.5873 0.1163 0.3038 408 1.6155 0.0806 0.3320 Table D18. Moisture gain/loss with respect to time Time Wt.change St.dev. Net wt.change hrs (8) (g) 0 4.1388 0.0667 0.0000 24 4.2868 0.0669 0.1481 48 4.2933 0.0745 0.1546 72 4.3024 0.0659 0.1637 96 4.3176 0.0653 0.1789 120 4.3058 0.0655 0.1671 144 4.3136 0.0622 0.1748 192 4.3244 0.0670 0.1856 240 4.3199 0.0682 0.1811 312 4.3230 0.0668 0.1843 360 4.3164 0.0676 0.1777 408 4.3162 0.0682 0.1775 156 Dimensioal Change(in) 0.4000 0.3500 ~ 0.3000 . 0.2500 0.2000 ~ 0.1500 0.1000 0.0500 0.0000 Dimensional changes(in) ,,_ £17,, + (Width)(in) thickness(in) -0.0500 0—190—499——300———499~——500 Time(hrs) Figure D6. Dimensional changes at 75% RH and 30°C. 157 Net weight Change at 75% RH and 30°C n . 1*:nst wt Clarissa 1 O 100 200 300 400 500 i Time (hrs) Figure D 7 Moisture gain/loss at 75% RH and 30°C. 158 Dimensional Changes and Moisture gain/loss with respect to time at 84% RH and 30°C. Table D19. Dimensional Changes data and moisture gain/loss at 84% and 30°C. Length 10/22/2003 10/23/2003 10/24/2003 25-Oct 10/27/2003 10/28/2003 Time hrs 0 24 48 72 96 120 84-B 2.0545 2.0315 2.004 1.9835 1.901 1.91 84-B-l 1.986 2.002 1.984 1.9835 1.876 1.8796 Ave. 2.027875 2.035 2.0225 2.009375 1.9495 1.950525 st.dev. [st.dev. 0.0279 0.0213 0.0345 0.0270 0.0629 0.0582 Width date 10/22/2003 10/23/2003 10/24/2003 25-Ocl 10/27/2003 10/28/2003 Time hrs 0 24 48 72 96 120 84-B 2.097 2.1 125 2.078 2.0405 1.98 1.9987 84-B-1 2.062 2.103 2.0685 2.055 2.0275 2.071 Ave. 2.02025 2.062125 2.048625 2.039 2.007125 2.023675 [st.dev. 0.07752298 0.07469302 0.067005014 0.04793094 0.053381147 0.07143383 Thickness Time date 10/22/2003 10/23/2003 10/24/2003 25-Oct 10/27/2003 10/28/2003 hrs 0 24 48 72 96 120 84-B 1.271 1.5305 1.5845 1.6165 1.66 1.6875 84-B-1 1.319 1.6175 1.6685 1.712 1.7765 1.7545 Ave.1" 1.295 1.574 1.6265 1.66425 1.71825 1.721 1" st.dev. 0.0339 0.0615 0.0594 0.0675 0.0824 0.0474 159 wt. change Time date 10/22/2003 10/23/2003 10/24/2003 25-Oct 10/27/2003 10/2 8/2003 hrs 0 24 48 72 96 120 84-B 3.7139 3.9096 3.9425 3.9574 3.9975 3.9886 84—B-1 4.0886 4.3005 4.3274 4.3452 4.3936 4.3837 ave. 1" ave.l" thickl thick 3.90125 4.10505 4.13495 4.1513 4.19555 4.18615 istdev. 0.2650 0.2764 0.2722 0.2742 0.2801 0.2794 (Continued from Table D19) 160 Length 10/29/2003 1 1/31/2003 11/2/2003 1 1/5/2003 1 1/7/2003 11/9/2003 Time hrs 144 192 240 3 12 360 408 84-B 1.8785 1.877 1.784 1.7625 1.724 1.7155 84-B-1 1.8335 1.8 1.7565 1.738 1.718 1.7065 Ave. 1.92625 1.920875 1.843125 1.825 1.8075 1.800375 st.dev. st.dev. 0.0730 0.0902 0.0746 0.0770 0.0878 0.0897 Width date 10/29/2003 1 1/31/2003 1 1/2/2003 11/5/2003 1 1/7/2003 1 1/9/2003 Time hrs 144 192 240 3 12 360 408 84-B 2.097 2.1 125 2.078 2.0405 1.98 1.9987 84-B-1 2.062 2.103 2.0685 2.055 2.0275 2.071 Ave. 2.0795 2.10775 2.07325 2.04775 2.00375 2.03485 st.dev. 0.0175 0.00475 0.00475 0.00725 0.02375 0.03615 Thicknes S Time date 10/29/2003 1 1/31/2003 1 1/2/2003 1 1/5/2003 1 1/7/2003 1 1/9/2003 84-B hrs 144 192 240 3 12 360 408 84-B-1 1.271 1.5305 1.5845 1.6165 1.66 1.6875 Ave.1" 1.319 1.6175 1.6685 1.712 1.7765 1.7545 1" 1.295 1.574 1.6265 1.66425 1.71825 1.721 st.dev. 0.0339 0.0615 0.0594 0.0675 0.0824 0.0474 wt. change Time date 10/29/2003 1 1/31/2003 1 1/2/2003 1 1/5/2003 1 1/7/2003 1 1/9/2003 84-B hrs 144 192 240 3 12 360 408 84cB-1 3.7139 3.9096 3.9425 3.9574 3.9975 3.9886 ave. 1" thick 4.0886 4.3005 4.3274 4.3452 4.3936 4.3837 ave. 1" thick 3.90125 4.10505 4.13495 4.1513 4.19555 4.18615 st.dev. 0.2650 0.2764 0.2722 0.2742 0.2801 0.2794 161 Table D 20. Change in Length with respect to time Time Length Net Change Date (hrs) (in) st.dev. Length(in) 10/22/2003 0 2.0279 0.0279 0.0000 10/23/2003 24 2.0350 0.0213 0.0071 10/24/2003 48 2.0225 0.0345 -0.0054 25-Oct 72 2.0094 0.0270 -0.0185 10/27/2003 96 1.9495 0.0629 -0.0784 10/28/2003 120 1.9505 0.05 82 -0.0773 10/29/2003 144 1.9263 0.0730 -0. 1016 1 1/31/2003 192 1.9209 0.0902 -0. 1070 1 1/2/2003 240 1.8431 0.0746 -0.1848 1 1/5/2003 312 1.8250 0.0770 -O.2029 11/7/2003 360 1.8075 0.0878 -0.2204 1 1/9/2003 408 1.8004 0.0897 -0.2275 Table D 21. Change in Width with respect to time Time Width Net chan e ‘ Date (hrs) (in) st.dev Width in) 10/22/2003 0 2.0203 0.0775 0.0000 10/23/2003 24 2.0621 0.0747 0.0419 10/24/2003 48 2.0486 0.0670 0.0284 25-Oct 72 2.0390 0.0479 0.0187 10/27/2003 96 2.0071 0.0534 -0.0131 10/28/2003 120 2.0237 0.0714 0.0034 10/29/2003 144 2.0229 0.0608 0.0026 1 1/31/2003 192 1.9941 0.0666 -0.0261 1 1/2/2003 240 1.941 1 0.0707 -0.0791 11/5/2003 312 1.9193 0.0767 -0.1010 1 1/7/2003 360 1.9036 0.0798 -0.1166 1 1/9/2003 408 1.8876 0.0825 -0. 1326 162 Table D 22. Change in Thickness with respect to time Time Thickness Net change Date (hrs) ' (in) st.dev. Thickness(in) 10/22/2003 0 1.2950 0.0339 0.0000 10/23/2003 24 1.5740 0.0615 0.2790 10/24/2003 48 1.6265 0.0594 0.3315 25-Oct 72 1.6643 0.0675 0.3693 10/27/2003 96 1.7183 0.0824 0.4233 10/28/2003 120 1.7210 0.0474 0.4260 10/29/2003 144 1.7255 0.0495 0.4305 11/31/2003 192 1.7450 0.0396 0.4500 1 1/2/2003 240 1.6688 0.0442 0.3738 11/5/2003 312 1.6610 0.0474 0.3660 11/7/2003 360 1.6560 0.0431 0.3610 11/9/2003 408 1.6788 0.0187 0.3838 Table 23: Moisture gain/loss with respect to time Time Wt. Change st.dev. Net wt.chan e Date (hrS) (g) (g) 10/22/2003 0 3.9013 0.2650 0.0000 10/23/2003 24 4.1051 0.2764 0.2038 10/24/2003 48 4.1350 0.2722 0.2337 25-Oct 72 4.1513 0.2742 0.2501 10/27/2003 96 4.1956 0.2801 0.2943 10/28/2003 120 4.1862 0.2794 0.2849 10/29/2003 144 4.1909 0.2760 0.2896 1 1/31/2003 192 4.1987 0.2790 0.2975 1 1/2/2003 240 4.2188 0.2782 0.3175 1 1/5/2003 312 4.2149 0.2788 0.3136 11/7/2003 360 4.2108 0.2747 0.3095 1 1/9/2003 408 4.2133 0.2757 0.3120 163 net dimensional change(ln) Dimensional Changes at 84% RH and 30°C Net weight Change(g Time (hrs) Figure D9. Moisture gain/loss 84% RH and 30°C. 164 l l l 1 l + Length(in) ; —I—- Width(in) l Thickness-1" i w l l __ _ _ _1 + Net wt.Change 1‘ l l l l l 1 l 4 Dimensional Changes and Moisture gain/loss with respect to time at 89% RH and 30°C. Table D 24. Dimensional Changes data and moisture gain/loss at 89% and 30°C. Length Date 10/22/200310/23/2003 10/24/2003 25-Oct 10/27/2003 10/28/2003 s.no. Time(hrs) 0 24 48 72 96 120 89-8 2.0105 1.3595 1.2665 1.2515 1.2483 1.231 89-B-1 2.1025 1.422 1.298 1.2835 1.2785 1.2545 Ave. 2.0565 1.39075 1.28225 1.2675 1.2634 1.24275 st.dev. 0.0650 0.0441 0.0222 0.0226 0.0213 0.0166 Width Date 10/22/200310/23/2003 10/24/2003 25-Oct 10/27/2003 10/28/2003 s.no Time(hrs) 0 24 48 72 96 120 89-B 1.9725 1.7795 1.715 1.694 1.685 1.6105 89-B-1 1.9805 1.3075 1.3012 1.2926 1.3875 1.385 Ave. 1.9765 1.5435 1.5081 1.4933 1.53625 1.49775 st.dev. 0.005 0.33 0.29 0.28 0.210 0.1594 Thickne SS Date 10/22/200310/23/2003 10/24/2003 25-Oct 10/27/2003 10/28/2003 s.no Time(hrs) O 24 48 72 96 120 , 89-B 1.3195 1.3025 1.2375 1.2815 1.2365 1.2255 ; 89-B-1 1.2896 1.2735 1.263 1.3205 1.316 1.273 1 Ave. 1.30455 1.288 1.25025 1.301 1.27625 1.24925 1 st.dev. 0.02 0.02 0.018 0.027 0.056 0.033 I wt. 01999 [ Date 10/22/200310/23/2003 10/24/2003 25—Oct 10/27/200310/28/20081 Is.no. Time(hrs) 0 24 4 72 96 120| [896 3.9087 4.3288 4.364 4.3813 4.5213 4.5181 5943-1 4.0355 4.4966 4.5325 4.5514 4.6855 4.673] lAve. 3.9721 4.4127 4.44825 4.46635 4.6034 4.5955] I st.dev. 0.09 0.118 0.12 0.12 0.12 0.11 | 165 (continued from table D24) Length Date 10/29/2003 1 1/31/2003 1 1/2/2003 1 1/5/2003 11/7/2003 11/9/2003 S.no. Time(hrs) 144 192 240 3 12 360 408 89-B 1.221 1.2295 1.2165 1.21 1 1.205 1.209 89-B-1 1.222 1.245 1.2295 1.2156 1.2365 1.239 Ave. 1.2215 1.23725 1.223 1.2133 1.22075 1.224 st.dev. 0.0007 0.01 10 0.0092 0.0033 0.0223 0.0212 Width Date 10/29/2003 1 1/31/2003 1 1/2/2003 1 1/5/2003 11/7/2003 1 1/9/2003 s.no Time(hrs) 144 192 240 312 360 408 89-B 1.5925 1.651 1.6075 1.5885 1.5465 1.5605 89-B-1 1.372 1.379 1.364 1.451 1.399 1.42 Ave. 1.48225 1.515 1.48575 1.51975 1.47275 1.49025 st.dev. 0.1559 0.1923 0.1722 0.0972 0.1043 0.0993 Thickness Date 10/29/2003 1 1/31/2003 11/2/2003 1 1/5/2003 11/7/2003 1 1/9/2003 s.no Time(hrs) 144 192 240 3 12 360 408 89-B 1.2315 1.256 1.2385 1.21 1.1654 1.2395 89-B-1 1.236 1.291 1.279 1.2085 1.198 1.2635 Ave. 1.23375 1.2735 1.25875 1.20925 1.1817 1.2515 st.dev. 0.0032 0.0247 0.0286 0.001 1 0.0231 0.0170 wt. change Date 10/29/2003 1 1/31/2003 1 1/2/2003 1 1/5/2003 1 1/7/2003 11/9/2003 s.no. Time(hrs) 144 192 240 3 12 360 408 89-B 4.5572 4.5542 4.6219 4.6083 4.6038 4.613 89-B-1 4.7035 4.732 4.7888 4.7874 4.789 4.785 Ave. 4.63035 4.6431 4.70535 4.69785 4.6964 4.699 st.dev. 0.1034 0.1257 0.1180 0.1266 0.1310 0.1216 166 Table D 25. Change in Length with respect to time Net changg_ Date Time(hrs) Lenfl st.dev. ngth 10/22/2003 0 2.0565 0.065054 0 10/23/2003 24 1.39075 0.044194 -0.6658 10/24/2003 48 1.28225 0.022274 -0.7743 25-Oct 72 1.2675 0.022627 -0.7890 10/27/2003 96 1.2634 0.021355 -0.7931 10/28/2003 120 1.24275 0.016617 -0.8 138 10/29/2003 144 1.2215 0.000707 -0.8350 11/31/2003 192 1.23725 0.01096 -0.8193 1 1/2/2003 240 1.223 0.009192 -0.8335 11/5/2003 312 1.2133 0.003253 -O.8432 1 1/7/2003 360 1.22075 0.022274 -0.8358 1 1/9/2003 408 1.224 0.021213 -0.8325 Table D26. Change in Width with respect to time Net change Date Time(hrs) Widt st.dev. Width 10/22/2003 0 1.9765 0.0057 0 10/23/2003 24 1 .5435 0.3338 -0.433 10/24/2003 48 1 .5081 0.2926 -0.4684 25-Oct 72 1 .4933 0.2838 -0.4832 10/27/2003 96 1 .53625 0.2104 -0.44025 10/28/2003 120 1 .49775 0.1595 -0.47875 10/29/2003 144 1 .48225 0.1559 -0.49425 11/31/2003 192 1.515 0.1923 -0.4615 1 1/2/2003 240 1 .48575 0.1722 -0.49075 1 1/5/2003 312 1 .51975 0.0972 -0.45675 1 1/7/2003 360 1 .47275 0.1043 -0.50375 1 1/9/2003 408 1 .49025 0.0993 -0.48625 167 Table D27. Change in Width with respect to time Time(hrs) Width Net change Date (hrs) (inL st.dev. Width(in) 10/22/2003 0 1.9765 0.0057 0 10/23/2003 24 1.5435 0.3338 -0.4330 10/24/2003 48 1.5081 0.2926 -0.4684 25-Oct 72 1.4933 0.2838 -0.4832 10/27/2003 96 1.5363 0.2104 -0.4403 10/28/2003 120 1.4978 0.1595 -0.4788 10/29/2003 144 1.4823 0.1559 -0.4943 11/31/2003 192 1.5150 0.1923 -0.4615 1 1/2/2003 240 1.4858 0.1722 -0.4908 1 1/5/2003 312 1.5198 0.0972 -0.4568 1 1/7/2003 360 1.4728 0.1043 -0.5038 1 1/9/2003 408 1.4903 0.0993 -0.4863 Table D28. Moisture gain/loss with respect to time Time (hrs) Thickness Net change Date (hrs) (in) st.dev. Thickness Q) 10/22/2003 0 1.3046 0.0211 0 10/23/2003 24 1.2880 0.0205 -0.0166 10/24/2003 48 1.2503 0.0180 -0.0543 25-Oct 72 1.3010 0.0276 -0.0035 10/27/2003 96 1.2763 0.0562 -0.0283 10/28/2003 120 1.2493 0.0336 -0.0553 10/29/2003 144 1.2338 0.0032 -0.0708 11/31/2003 192 1.2735 0.0247 -0.0311 11/2/2003 240 1.2588 0.0286 -0.0458 11/5/2003 312 1.2093 0.0011 -0.0953 11/7/2003 360 1.1817 0.0231 -0. 1229 11/9/2003 408 1.2515 0.0170 -0.0531 168 i Dimensional Changes at 89%RH and 30°C l i 0.0000 '9‘ r 4 t v ? -0.1000 —— -.__ 100 ——200 e 4300 —— ——400 500 ‘5' _ ___. d) U c , 7 . 2 M ‘ + Length ‘7: +Width 5 Thickness '3 — *’ “—‘" C 43 _ 2 .15. o 1 Figure D10. Dimensional changes at 89% RH and 30°C. 1 1 Net Wt.Change at 89% RH and 30C 1 1+ NetWt:.9rw;ge<9> Net Weight gain (9) 0 100 200 300 400 500 Time (hrs) Figure D 11. Moisture gain/loss at 89% RH and 30°C. 169 Dimensional Changes and Moisture gain/loss with respect to time at 95% RH and 30°C. Table D29. Dimensional Changes data and moisture gain/ loss at 95% and 30°C. Length 10/22/2003 10/23/2003 10/24/2003 25-Oct 10/27/2003 10/28/2003 S.no. Time(hrs) 0 24 48 72 96 120 95-8 2.017 1.298 1.2525 1.2155 1.1575 1.1495 95-B-1 2.0675 1.244 1.2225 1.189 1.1635 1.1205 Ave. Length 2.04225 1.271 1.2375 1.20225 1.1605 1.135 St Dev. 0.0357 0.0382 0.0212 0.0187 0.0042 0.0205 Width date 10/22/2003 10/23/2003 10/24/2003 25-Oct 10/27/2003 10/28/2003 s.no hrs 0 24 48 72 96 120 95—B 2.114 1.521 1.443 1.415 1.393 1.3575 95-B-1 1.965 1.6395 1.6015 1.564 1.5615 1.548 Ave. Width 2.0395 1.58025 1.52225 1.4895 1.47725 1.45275 St Dev. 0.1054 0.0838 0.1121 0.1054 0.1191 0.1347 Thickne 53 Days 10/22/2003 10/23/2003 10/24/2003 25-Oct 10/27/2003 10/28/2003 s.no 95-B 1.293 1.3205 1.267 1.2255 1.2005 1.1985 95-B-1 1.2435 1.2995 1.223 1.2185 1.2035 1.2 Thicknes Ave. S 1.26825 1.31 1.245 1.222 1.202 1.19925 St Dev. 0.0350 0.0148 0.0311 0.0049 0.0021 0.0011 wt. change Days 110/22/2003 10/23/2003 10/24/2003 25-Oct 10/27/2003 10/28/2003 s.no. 95-B 3.827 4.2351 4.2606 4.326 4.4378 4.4707 95-B-1 3.8273 4.2501 4.3056 4.345 4.4773 4.469 Wt. Ave. Change 3.82715 4.2426 4.2831 4.3355 4.45755 4.46985 St Dev. 0.0002 0.0106 0.0318 0.0134 0.0279 0.0012 170 (continued from Table D29) Length . 10/29/2003 1 1/31/2003 1 1/2/2003 1 1/5/2003 1 1/7/2003 1 1/9/2003 s.no. Timefitrs) 144 192 240 312 360 408 95-B 1.146 1.1435 1.176 1.17 1.1685 1.167 95—B-1 1.112 1.1085 1.2445 1.217 1.204 1.1885 Ave. Length 1.129 1.126 1.21025 1.1935 1.18625 1.17775 St Dev. 0.0240 0.0247 0.0484 0.0332 0.0251 0.0152 Width date 10/29/2003 1 1/31/2003 1 1/2/2003 11l5/2003 1 1 /7/2003 1 1/9/2003 s.no hrs 144 192 240 312 360 408 95-B 1.3555 1.3825 1.453 1.419 1.381 1.3885 95-B-1 1.53 1.537 1.5495 1.5245 1.4965 1.5365 Ave. Width 1.44275 1.45975 1.50125 1.47175 1.43875 1.4625 St Dev. 0.1234 0.1092 0.0682 0.0746 0.0817 0.1047 Thickne ss Days 10/29/2003 1 1/31/2003 11/2/2003 1 1/5/2003 1 1/7/2003 1 1/9/2003 s.no 144 192 240 312 360 408 95-B 1.192 1.196 1.216 1.21 1.218 1.2165 95-B-1 1.186 1.178 1.1935 1.19 1.2075 1.209 Thicknes Ave. 3 1.189 1.187 1.20475 1.2 1.21275 1 .21275 St Dev. 0.0042 0.0127 0.0159 0.0141 0.0074 0.0053 wt. change 1 Days 10/29/2003 1 1/31/2003 11/2/2003 1 1/5/2003 1 1/7/2003 1 1/9/2003 s.no. 95—B 4.4739 4.4985 4.6515 4.6089 4.668 4.6593 95—B-1 4.4639 4.4721 4.6433 4.592 4.7501 4.6593 Wt. Ave. Change 4.4689 4.4853 4.6474 4.60045 4.70905 4.6593 St Dev. 0.0071 0.0187 0.0058 0.0120 0.0581 0.0000 171 Table D 30. Change in Length with respect to time Net change Date Time(hrs) Length St Dev. (length) 10/22/2003 0 2.0423 0.0357 0 10/23/2003 24 1.2710 0.0382 -0.7713 10/24/2003 48 1.2375 0.0212 -0.8048 25-Oct 72 1.2023 0.0187 -0.8400 10/27/2003 96 1 . 1605 0.0042 -0.8818 10/28/2003 120 1.1350 0.0205 -0.9073 10/29/2003 144 1.1290 0.0240 -0.9133 1 1/31/2003 192 1.1260 0.0247 -0.9163 11/2/2003 240 1.2103 0.0484 -0.8320 11/5/2003 312 1.1935 0.0332 -0.8488 11/7/2003 360 1.1863 0.0251 -0.8560 1 1/9/2003 408 1.1778 0.0152 -0.8645 Table D 31: Change in Width with respect to time Time Width Net change Date (hrs) (in) St Dev.(width) width (in) 10/22/2003 0 2.0395 0.1054 0 10/23/2003 24 1.5803 0.0838 -0.4593 10/24/2003 48 1.5223 0.1121 -0.5173 25-Oct 72 1.4895 0.1054 -0.5500 10/27/2003 96 1.4773 0.1191 -0.5623 10/28/2003 120 1.4528 0.1347 -0.5868 10/29/2003 144 1.4428 0.1234 -0.5968 11/31/2003 192 1.4598 0.1092 -0.5798 1 1/2/2003 240 1.5013 0.0682 -0.5383 11/5/2003 312 1.4718 0.0746 -0.5678 11/7/2003 360 1.4388 0.0817 -0.6008 1 1/9/2003 408 1.4625 0.1047 -0.5770 172 Table D32. Change in Thickness with respect to time Time Thickness Net change Date (hrs) (in) St Dev. thickness(in) 10/22/2003 0 1.2683 0.0350 0 10/23/2003 24 1.3100 0.0148 0.0417 10/24/2003 48 1.2450 0.031 1 -0.0233 25-Oct 72 1.2220 0.0049 -0.0463 10/27/2003 96 1.2020 0.0021 -0.0663 10/28/2003 120 1.1993 0.001 1 -0.0691 10/29/2003 144 1.1890 0.0042 -0.0793 11/31/2003 192 1.1870 0.0127 -0.0813 1 1/2/2003 240 1.2048 0.0159 -0.0636 1 1/5/2003 312 1.2000 0.0141 -0.0683 1 1/7/2003 360 1.2128 0.0074 -0.0556 11/9/2003 408 1.2128 0.0053 -0.0556 Table 33: Moisture gain/loss with respect to time Net wt. Time Wt. Change change Date (hrs) (g) St Dev. (g) 10/22/2003 0 3.8272 0.0002 0 10/23/2003 24 4.2426 0.0106 0.4154 10/24/2003 48 4.2831 0.0318 0.4560 25-Oct 72 4.3355 0.0134 0.5084 10/27/2003 96 4.4576 0.0279 0.6304 10/28/2003 120 4.4699 0.0012 0.6427 10/29/2003 144 4.4689 0.0071 0.6418 11/31/2003 192 4.4853 0.0187 0.6582 1 1/2/2003 240 4.6474 0.0058 0.8203 11/5/2003 312 4.6005 0.0120 0.7733 11/7/2003 360 4.7091 0.0581 0.8819 1 1/9/2003 408 4.6593 0.0000 0.8322 173 Dimensioal changes at 95%RH and 30°C 1 0.2000 , _ ,- ,. i % 0.0000 [ . r . 4 1 8' 02000 , ' )0 i g + Net Change(length) 7' -0.4000 < 7‘ + Net change(width) 5 _0_6000 - _ , . . Njflwfliflmfifl E 1 E -0.8000 9 ‘ E 1 -1.0000 ‘ Figure D 12. Dimensional changes at 95% RH and 30°C. P V net wt. change ( ) 0 100 200 300 Time(hrs) 400 500 Net weight change at 95% Rh and 30°C + Net wt. change ———'_’ ' __ ' l Figure D13. Moisture loss/gain at 95% RH and 30°C. 174 APPENDIX C MOISTURE SENSITIVITY 0G GREEN CELL® FOAM Initial Moisture Content "Mi" calculations Table M . Initial moisture Content Calculations of Green Cell® foam after Wt. of Sample Dish Wt Wt.of Wt. of heating product Wt. of Mi No. (g) product+ roduct before dish after product after (g) dish before heating (g) heating (g) heating(g) heating ssl 1.2711 2.0412 0.7701 4.6269 1.9274 0.6563 0.1734 952 1.2745 2.0023 0.7278 4.8564 1.9028 0.6283 0.1584 553 1.2717 2.0148 0.7431 1.9173 0.6456 0.1510 554 1.2821 1.9012 0.6191 1.8485 0.5664 0.0930 555 1.2755 1.9086 0.6331 1.8556 0.5801 0.0914 336 1.2734 1.9092 0.6358 4.7730 1.8563 0.5829 0.0908 Sum 11.7773 4.1290 14.2563 11.3079 3.6596 0.7579 Ave. 1.9629 0.6882 Avg 1.8847 0.6099 0.1263 Ave. 0.1263 Mi 0.1263 175 Experimental Moisture Content “Me” Calculations at 20°C and different humidity conditions. Table M 1. Experimental Moisture Content “Me” Calculations at 20°C and different humidity conditions. Date : 1 1/12/2003 1 1/13/2003 1 1/14/2003 SNO. %RH PAN Salt PAN Wt Pan + Prod Pan+ prod No. Name gm gm (RI) Lithium 1 l 1 Licl-sal Chloride 1.2788 1.7795 1.7595 1.7602 2 532 1.2686 1.7936 1.7687 1.769 3 383 1.2782 1.7716 1.7541 1.7563 KC2H302- 4 21 sal Potassium 1.2744 1.7697 1.7582 1.7586 5 sa2 Acetate 1.2656 1.75 1.7395 1.7394 6 583 1.2743 1.7855 1.7745 1.7749 7 34 MgC 12-sa1 magnesium 1.2695 1.7348 1.7274 1.727 8 332 Chloride 1.2704 1.7497 1.7494 1.7437 9 sa3 1.272 1.7564 1.7434 1.7494 Mg(NO3)2- 10 55 sal magnesium 1.2698 1.7636 1.7662 1.7661 11 sa2 Nitrate 1.2856 1.7888 1.7914 1.7916 12 sa3 1.2743 1.764 1.7662 1.7663 13 63 NaNO3-sal Sodium Nitrate 1.2643 1.7562 1.7634 1.7645 14 sa-2 1.282 1.758 1.765 1.7658 15 sa-3 1.2757 1.7608 1.7673 1.7685 7200 16 % NaCl-sal Sodium 1.2637 1.7507 1.7782 1.7808 17 582 Chloride 1.2742 1.7777 1.8062 1.8093 18 sa3 1.2699 1.7807 1.8103 1.8113 19 83 KCl-sal Potassium 1 .2 763 1.7955 1.8431 1.8438 20 sa2 Chloride 1.2764 1.7563 1.7989 1.7992 21 sa3 1.2756 1.7873 1.8328 1.8335 22 96 K2SO4- sal Potassium 1.2689 1.772 1.913 1.9074 23 kclsa2 Sulphate 1.268 1.7625 1.9149 1.8944 24 kclsa3 1.2805 1.7752 1.9016 1.9008 176 (continued from Table M 1) Date : SNO. PAN No. Licl-sal sa2 sa3 sa2 883 $32 sa3 O3 sa2 sa3 \OOOQONLIIDWN— I—Ib—nlu—lI-I- LAN—O sa-2 sa-3 t—Dt—iI—l OLA-b saZ sa3 ——O— 000% sa2 sa3 NNN N—‘O kclsaZ kclsa3 rJN Aw KC2H302-sal M -sa1 NaNO3-sal 7200% NaCl-sal KCl-sal KZSO4- sal Lithium Chloride Sodium Nitrate 177 (continued from table M 1.) Date : 1 1/17/03 11/19/03 1 1/21/03 11/24/03 SNO. %RH PAN Salt No. Name Lithium 1 1 1 Licl-sal Chloride 1.7637 1.7643 1.7627 1.7632 2 sa2 ' 1.7702 1.7712 1.7703 1.7715 3 383 1.7583 1.7587 1.758 1.7588 4 21 KC2H302-sal Potassium 1.7592 1.7592 1.7599 1.758 5 sa2 Acetate 1.7403 1.7405 1.7393 1.7383 6 sa3 1.7764 1.7764 1.7757 1.7743 7 34 MgCl2-sal Magnesium 1.7271 1.7278 1.7278 1.727 8 $82 Chloride 1.7434 1.7435 1.7428 1.7427 9 583 1.7492 1.75 1.7492 1.7493 10 55 M g(NO3)2-sa 1 Magnesium 1.7664 1.7664 1.7664 1.7663 11 sa2 Nitrate 1.7917 1.7918 1.792 1.792 12 533 1.7666 1.7668 1.7668 1.7667 Sodium 13 63 NaNO3-sal Nitrate 1.7657 1.7662 1.7659 1.7661 14 sa-2 1.7666 1.7689 1.7675 1.7676 15 sa-3 1.7701 1.7705 1.7703 1.7705 16 7200% NaCl-sal Sodium 1.781 1.7825 1.7815 1.7823 17 sa2 Chloride 1.8094 1.81 1.8098 1.8106 18 583 1.8114 1.8116 1.811 1.8127 19 83 KCl-sal Potassium 1.842 1.8412 1.8411 1.841 20 sa2 Chloride 1.7985 1.7981 1.7985 1.7986 21 sa3 1.8327 1.8321 1.832 1.8321 22 96 K2SO4- sal Potassium 1.9256 1.917 1.9216 1.8805 23 kclsa2 Sulphate 1.9133 1.903 1.9076 1.8681 24 kclsa3 1.9242 1.9142 1.9188 1.8786 178 (continued from table M1) Date : 1 1/27/2003 1 1/30/2003 12/4/2003 SNO. %RH PAN Salt No. Name 1 11 Licl-sal Lithium Chloride 1.765 1.7682 1.7677 2 sa2 1.7753 1.7784 1.7759 3 383 1.7645 1.7671 1.7639 4 21 KC2H302-sal Potassium 1.7589 1.7585 1.7576 5 sa2 Acetate 1.7401 1.7396 1.739 6 sa3 1.7784 1.7758 1.7749 7 34 M gClZ-sal magnesium 1.7273 1.7288 1.7277 8 $32 Chloride 1.7434 1.7438 1.7421 9 583 1 .7499 1.7503 1.7494 10 55 M gQ‘l O3)2-sal magnesium 1.7666 1.7666 1.7665 1 l sa2 Nitrate 1.7922 1.7923 1.7916 12 583 1.7668 1.7678 1.7666 13 63 NaNO3—sal Sodium Nitrate 1.7662 1.7667 1.7671 14 sa-2 1.7677 1.7685 1.7689 15 sa-3 1.7708 1.772 1.7725 16 7200% NaCl-sal Sodium 1.7834 1.7839 1.7828 17 sa2 Chloride 1.8109 1.8115 1.8097 18 sa3 1.8135 1.8151 1.8132 19 83 KC l-sa 1 Potassium 1.8431 1.843 1.844 20 882 Chloride 1.8007 1.801 1.8022 21 sa3 1.8333 1.8335 1.8377 22 96 K2SO4- sal Potassium 1.9028 1.9017 1.8562 23 kclsa2 Sulphate 1.8895 1.8887 1.8876 24 kclsa3 1.9036 1.9025 1.8612 179 (Continued from table M 1) Date : 12/8/2003 12/15/2003 SNO. %RH PAN Salt No. Name 1 1 1 Licl-sal Lithium Chloride 1.736 1.7659 2 532 1.7737 1.7794 3 sa3 1.7612 1.7672 4 21 KC2H302-sal Potassium 1.758 1.7573 5 $82 Acetate 1.7392 1.738 6 sa3 1.7749 1.7738 7 34 MgClZ-sal magnesium 1.7273 1.7276 8 582 Chloride 1.7422 1.7425 9 sa3 1.7494 1.749 10 55 M g(NO3)2-sa1 magnesium 1.7669 1.7673 1 1 sa2 Nitrate 1.7916 1.7922 12 583 1.7665 1.7671 13 63 NaNO3-sal Sodium Nitrate 1.7665 1.7663 14 sa-2 1.768 1.7682 15 sa-3 1.7715 1.7713 16 7200% NaCl-sal Sodium 1.7819 1.7821 17 532 Chloride 1.809 1.811 18 sa3 1.8126 1.8124 19 83 KC l-sa 1 Potassium 1.8421 1.8464 20 sa2 Chloride 1.8009 1.8054 21 sa3 1.835 1.8403 22 96 KZSO4- 53] Potassium 1.9643 2.0065 23 kclsa2 Sulphate 1.9597 1.9954 24 kclsa3 1.9075 1.989 Fungus Fungus 180 (continued from Table M 1) %RH PAN Salt No. Name Ange Wi Avg Wi %RH Me Aw w/Me Lithium 11 LicI-sa1 Chloride 0.5007 0 0 0 0 sa2 0.525 sa3 0.4943 0.4934 0.5064 11 0.0995 0.11001.1051 KC2H302- 21 sa1 Potassium 0.4953 532 Acetate 0.4844 sa3 0.4849 0.5112 0.4970 21 0.0990 0210021206 34 MgCl2-sa1 magnesium 0.4653 332 Chloride 0.4793 sa3 0.4691 0.4844 0.4763 34 0.109103400311591 Mg(NO3)2- 1 55 sa1 magnesium 0.4938 sa2 Nitrate 0.5032 | 533 0.4990 0.4897 0.4956 55 0.1340 05500410361 63 NaNOB-sa1 Sodium Nitrate 0.4919 sa-2 0.476 sa-3 0.4946 0.4851 0.4843 63 0.1502 0630041951 7200 % NaCl-sa1 Sodium 0.487 s32 Chloride 0.5035 833 0.5326 0.5108 0.5004 0.72 0.1986 0720036250 83 KCl-sa1 Potassium 0.5192 332 Chloride 0.4799 633 0.5546 0.5117 0.5036 83 02404 0830034531 96 K2804-sa1 Potassium 0.5031 kcI-sa2 Sulphate 0.4945 kcl-sa3 0.5959 0.4947 0.4974 96 0.3492 0.9600 .7493 GAB model constants and T ,C Wm and K Values: (X B Y T C Wm K = -11.089 = 13.525 = -0.1353 -117.92 = 0.9917,-118.9143 -0.0752, 0.0752 99.1363 181 RMS calculations. Table M 2. RMS calculation for GAB model at 20°C and different %RH conditions Aw CkAw (1-kAw).. M (Gab) M (Exp) 0 0 0 0 0.11 10.8141 -9.0042 0.0903 0.0995 0.0925 0.0086 0.21 20.6450 -16.3779 0.0948 0.0990 0.0427 0.0018 0.34 33.4253 -23.5130 0.1069 0.1091 0.0206 0.0004 0.55 54.0703 -29. 1872 0.1393 0.1340 -0.0392 0.0015 0.63 61.9350 -29.4473 0.1581 0.1502 -0.0530 0.0028 0.72 70.7829 -28.4860 0.1868 0.1986 0.0595 0.0035 0.83 81.5970 -25.5080 0.2405 0.2404 -0.0006 0.0000 0.96 94.3772 -19.4315 0.3651 0.3490 -0.0463 0.0021 0.0026 RMS 5.1025 182 Experimental Moisture Content “Me” Calculations at 25°C and different humidity conditions. Table M 3. Experimental Moisture Content “Me” Calculations at 25°C and different humidity conditions. Date : 7/7/2003 7/7/2003 7/8/2003 SNO. %RH PAN Salt PAN Wt Pan + Prod Pan+ prod No. Name gm gm (R1) 1 15 Licl-sal Lithium 1.2748 2.0449 1.9968 1.995 2 sa2 Chloride 1.2737 2.0261 1.9825 1.9786 3 583 1.2726 2.0386 1.9906 1.9883 4 23 1((C2 H302)-sa1 Potassium 1.2708 2.0291 1.9971 1.9966 5 sa2 Accetate 1.2684 2.0295 1.993 1.991 6 sa3 1.2748 2.1493 2.1104 2.1076 7 35 MgCl-sal Magnesium 1.2732 2.02 1.9889 1.9885 8 $82 Chroride 1.2739 2.026 1.9931 1.9922 9 sa3 1.275 2.0126 1.9829 1.982 10 51 Mg(NO3)2-sa1 Magnesium 1.2666 2.0123 2.0069 2.0057 1 1 582 Chloride 1.2785 2.004 1.9979 1.9968 12 sa3 1.2834 2.0199 2.0124 2.0115 13 63 NaNoZ-sal Sodium 1.2719 2.0168 2.0166 2.0161 14 $82 Nitride 1.2753 2.0207 2.02 2.0193 15 sa3 1.2725 2.0313 2.0308 2.0305 16 73 Naclsal Sodium 1.2732 2.0371 2.0728 2.0744 17 Naclsa2 C hroride 1.2746 2.0016 2.0295 2.0309 18 NaClsa3 1.2737 2.016 2.0455 2.0469 19 84 kc] -sa1 Potassium 1.2755 2.0182 2.0928 2.0912 20 kcl-saZ Chloride 1.2717 2.0024 2.0769 2.081 21 kcl-sa3 1.2797 2.01 14 2.0886 2.0902 183 (continued from table M3) Date : 7/9/2003 7/10/2003 7/1 1/2003 SNO. %RH PAN Salt No. Name 1 15 Licl-sa 1 Lithium 1.9944 1.9946 1.9946 2 sa2 Chloride 1.9782 1.9784 1.9773 3 sa3 1.9888 1.9891 1.9873 4 23 K(C2H302)-sa1 Potassium 1.9949 1 .9975 1.9931 5 sa2 Accetate 1.9906 1.992 1.9896 6 sa3 . 2.1073 2.1114 2.1057 7 35 MgC 1-sa1 Magnesium 1.9875 1.9877 1.9863 8 $82 Chroride 1 .9904 1 .9907 1.9802 9 sa3 1.9812 1.9816 1.9801 10 5 1 Mg(NO3)2-sa 1 Magnesium 2.0047 2.0049 2.0032 1 1 $82 Chloride 1.9966 1.9966 1 .9949 12 sa3 2.011 2.011 2.0094 13 63 NaNoZ-sal Sodium 2.015 2.0152 2.0146 14 sa2 Nitride 2.0186 2.0184 2.0178 15 sa3 2.0297 2.0073 2.007 16 73 Naclsal Sodium 2.073 2.0733 2.0705 17 NaclsaZ Chroride 2.0306 2.0297 2.0282 18 NaClsa3 2.0462 2.047 2.0453 19 84 kc] -sa1 Potassium 2.088 2.0802 2.0802 20 kcl—sa2 Chloride 2.0762 2.0656 2.066 21 kcl-sa3 2.0822 2.0754 2.0721 184 (continued from Table M3) 7/ 1 2/03/ 7/1 3/03/ 7/1 2/03/ 7/14/03/ SNO. %RH PAN Salt Pan + Prod Pan + Prod Pan + Prod Pan + Prod No. Name m (R2) Fm (R2) Em (R2) (m (R2) 1 15 Licl-sal Lithium 1.9929 0.7181 1.993 0.7182 2 sa2 Chloride 1 .9761 0.7024 1.9765 0.7028 3 sa3 1.9863 0.7137 1.9871 0.7145 4 23 K(C2H302)-sa1 Potassium 1.9927 0.7219 1.9929 0.7221 5 sa2 Accctate 1 .9887 0.7203 1 .9898 0.7214 6 583 2.1047 0.8299 2.105 0.8302 7 35 MgCl-sal Magnesium 1.9869 0.7137 1.9886 0.7154 8 sa2 Chroride 1 .9898 0.7159 1 .9906 0.7167 9 sa3 1 .9805 0.7055 1.9819 0.7069 10 51 Mg(NO3)2-sa1 Magnesium 2.004 0.7372 2.0038 2.0038 1 1 sa2 Chloride 1.9959 0.717 1.9955 1.9956 12 sa3 2.0105 0.7266 2.01 2.0101 13 63% NaNoZ-sal Sodium 2.0156 0.7437 2.0161 0.7442 14 sa2 Nitride 2.0189 0.7436 2.0185 0.7432 15 583 2.0079 0.7354 2.0083 0.7358 16 73 Naclsal Sodium 2.0725 0.7993 2.0726 0.7994 17 Naclsa2 Chroride 2.0298 0.7552 2.0298 0.7552 18 NaClsa3 2.0726 0.7989 2.0472 0.7735 19 84 kc] -sal Potassium 2.0882 0.8127 2.0854 2.0902 20 kcl-sa2 Chloride 2.0694 0.7977 2.075 2.0759 21 kcl-sa3 2.078 0.7983 2.0792 2.0804 185 (continued from table M3) 7/15/2003 7/17/2003 SNO. %RH PAN Salt Pan + Prod No. Name 1 15 Licl-sal Lithium 1.9923 1.9929 2 sa2 Chloride 1.766 1.9756 3 sa3 1.986 1.986 4 23 1((C 2H302)-sa1 Potassium 1.9932 1.9932 5 sa2 Accetate 1.9892 1.9892 6 sa3 2.105 2.1047 7 35 MgCl-sal Magnesium 1.967 1.9866 8 $32 Chroride 1.991 1.9898 9 583 1.981 1 1.9806 10 5 1 Mg(NO3)2-sa 1 Magnesium 2.004 2.004 1 1 sa2 Chloride 1.9957 1.9956 12 sa3 2.01 2.0104 13 63% NaNoZ-sal Sodium 2.0153 2.0152 14 sa2 Nitride 2.0184 2.0182 15 sa3 2.0081 2.0079 16 73 Naclsal Sodium 2.0723 2.0722 17 NaclsaZ Chroride 2.0292 2.029 18 NaClsa3 2.046 2.0461 19 84 kcl -sal Potassium 2.0876 2.1044 20 kcl-sa2 Chloride 2.0771 2.077 21 kcl-sa3 2.0826 2.0825 186 (continued from M3) % RH PAN Salt SD 8.0 Ave. Ave. 8.0 No. Name We We (We) (We) Wi Wi Wi (wi) 15 LicI-sa1 Lithium 0.718 0.770 sa2 Chloride 0.701 0.752 sa3 0.713 0.711 0.0083 0.0083 0.762 0.766 0.7628 0.0093 K(CZH302)- 23 sa1 Potassium 0.722 0.758 sa2 Accetate 0.720 0.761 sa3 0.829 0.757 0.0625 0.0625 0.797 0.874 0.7980 0.0663 35 MgCl-sa1 Mamesium 0.713 0.746 sa2 Chroride 0.715 0.752 sa3 0.705 0.711 0.005 0.0054 0.745 0.737 0.7455 0.0073 51 Mg(N03)2 Magesium 0.737 0.746 582 Chloride 0.717 0.725 sa3 0.727 0.727 0.010 0.0102 0.745 0.736 0.7450 0.0103 63 NaNoZ-sa1 Sodium 0.743 0.744 882 Nitride 0.742 0.745 sa3 0.735 0.740 0.004 0.0045 0.749 0.758 0.7497 0.0079 73 Naclsa1 Sodium 0.79 0.763 Naclsa2 Chroride 0.754 0.727 NaClsa3 0.772 0.775 0.022 0.0224 0.744 0.742 0.7444 0.0185 84 kcl-sa1 Potassium 0.828 0.742 kcl-$32 Chloride 0.805 0.730 kcl-saa 0.802 0.812 0.014 0.0144 0.735 0.731 0.7350 0.0067 187 (continued from M3) %RH Me (separate) Me Aw Aw/Me 0 0.0502 0 0 0 0.0507 15 0.0490 0.0499665 0.15 3.00200912 0.0730 0.0667 23 0.0689 0.0694651 0.23 3.31101463 0.0759 0.0721 35 0.0774 0.0751343 0.35 465832494 0.1129 0.1128 51 0.1115 0.0993394 0.51 5.13391716 0.1239 0.1225 63 0.0916 0.1125286 0.63 559857659 0.1781 0.1687 73 0.1720 0.1730022 0.73 4.21959923 0.2570 0.2413 84 0.2357 0.2447477 0.84 3.43210614 GAB model constants and T ,C Wm and K Values: -18.971 19.935 0.0619 342.417 341.4136 , 1.0029 0.0499, -0.0499 0.9488 188 FF RMS Calculations Table M 4. RMS calculation for GAB model at 25°C and different %RH conditions Aw CkAw (1-kAw).. MQGabJ M(Exp) 0 0 0 0.15 48.5924 42.4120 0.0571 0.0501 -0.1401 0.0196 0.23 74.5084 58.8592 0.0631 0.0695 0.0917 0.0084 0.35 113.3823 76.1745 0.0742 0.0760 0.0233 0.0005 0.51 165.2142 85.5314 0.0963 0.0993 0.0299 0.0009 0.63 204.0881 82.2514 0.1237 0.1125 —0.0999 0.0100 0.73 236.4831 72.7755 0.1620 0.1730 0.0633 0.0040 0.84 272.1175 55.2724 0.2455 0.2447 -0.0033 0.0000 0.0062 RMS 7.8810 189 Experimental Moisture Content “Me” Calculations at 30°C and different humidity conditions. Table M 5. Experimental Moisture Content “Me” Calculations at 30°C and different humidity conditions. Date: 10/22/2003 10/23/2003 10/24/2003 SNO. %RH PAN Chemical PAN Wt Pan + Prod Pan+ prod Pan+ prod No. Name L g (Q (9L 1 1 1 Licl-sa1 Lithium 1 .2742 1 .7724 1.7587 1.7576 2 sa2 Chloride 1 .2823 1.7839 1 .7696 1.769 3 sa3 1 .2746 1 .8024 1 .7882 1.7865 4 45 K2003-sa1 Potassium 1 .271 1 .7585 1 .7559 1 .7552 5 sa2 Carbonate 1 .2761 1 .7894 1 .7863 1 .786 6 333 1.2691 1.7469 1.7441 1.7443 7 56 MgZNo3-sa1 Magnesium 1.2743 1.7207 1.7231 1.7238 8 $32 Nitrate 1 .2813 1.7587 1.761 1.7621 9 sa3 1 .2633 1.7577 1.7608 1.7619 10 77 Nacl-sa1 Sodium 1 .2639 1 .7227 1.7395 1.74 1 1 sa2 Chloride 1 .2664 1 .7683 1 .7882 1.7897 12 $33 1 .2756 1 .7563 1.7746 1 .7763 13 8400% Kcl-sa1 Potassium 1.2692 1.7522 1.7822 1.7856 14 sa2 Chroride 1.273 1 .7482 1.7773 1 .7833 15 sa3 1 .2827 1 .7695 ‘l .798 1.8024 16 90 K2No3-sa1 Potassium 1 .2799 1 .7678 1.8237 1.8279 17 $32 Nitrate 1.2754 1.7563 1.8109 1.8147 18 333 1.2728 1.777 1.8321 1.8382 19 96 K2so4- sa1 Potassium 1.277 1.7766 1.8346 1.853 kclsaZ Sulphate 1.2755 1.7724 1.8273 1.8516 kclsa3 1 .2809 1 .7942 1 .8546 1 .8744 190 (continued from table M5) Date : 10/2 5/2003 10/27/2003 10/28/2003 10/29/2003 SNO. °/o RH PAN Chemical No. Name 1 1 1 Licl-sa1 Lithium 1 .7577 mfd 2 sa2 Chloride 1 .7678 1 .7595 1 .7558 1.7564 3 sa3 1 .7864 1 .7857 1 .7809 1 .7823 4 45 K2C03-sa1 Potassium 1 .755 1 .7551 1 .7539 1.7547 5 $32 Carbonate 1 .785 1 .7853 1.7849 1 .7852 6 533 1.7437 1.7438 1.7433 1.7432 M92N03- 7 56 sa1 Magnesium 1.723 1 .7225 1.724 1 .723 8 sa2 Nitrate 1.7613 1 .7628 1 .7613 1 .7608 9 sa3 1.7605 1.7625 1.7619 1.7606 10 77 NaCI-sa1 Sodium 1.7404 1.742 1.7423 1.7419 1 1 $32 Chloride 1 .7892 1.791 1.7909 1.7906 12 sa3 1 .7772 1 .7778 1.7773 1.7769 13 8400 KCl-sa1 Potassium 1.7864 1.7902 1 .7904 1 .7924 14 $32 Chroride 1.7845 1.7875 1.785 1.788 15 333 1.8037 1.8056 1.806 1.808 16 90 K2N03-sa1 Potassium 1.8314 1.852 1.844 1.8494 17 sa2 Nitrate 1 .8189 1 .8393 1.8306 1.8361 18 533 1.8416 1.8573 1.8535 1.8561 19 96 K2804- sa1 Potassium 1.8564 1.8643 1.8576 1.8623 KCIsaZ Sulphate 1 .855 1 .8624 1.8597 1.8593 KClsa3 1 .8812 1 .8832 1.8806 1.8839 191 (continued from table M5) Date : 10/30/2003 11/2/2003 11/3/2003 11/5/2003 SNO. %RH PAN Chemical No. Name 1 11 Licl-sa1 Lithium 2 $32 Chloride 1.7604 1.7915 1.7627 1.7532 3 533 1.787 1.7972 1.788 1.788 4 45 K2C03-sa1 Potassium 1 .7554 1 .7547 1.7538 1.7536 5 sa2 Carbonate 1.7858 1 .7854 1.7852 1 .7845 6 sa3 1.7439 1.7438 1.7436 1.7436 7 56 Mflo3-sa1 Magnesium 1.7233 1.7224 1.728 1.726 8 sa2 Nitrate 1 .7623 1 .7609 1.7613 1 .761 9 sa3 1.7614 1.7605 1.7598 1.7603 10 77 Nacl-sa1 Sodium 1.7438 1.743 1.7428 1.7424 11 sa2 Chloride 1.7918 1.7921 1.7921 1.7923 12 sa3 1.7798 1 .7784 1.7782 1.7782 13 8400% Kcl-sa1 Potassium 1 .7915 1 .7932 1 .7958 1.7972 14 sa2 Chroride 1.788 1 .7888 1.7891 1.7978 15 sa3 1.808 1.81 1.811 1.8099 16 90 K2No3-sa1 Potassium 1.8506 1 .8615 1.8661 1.86 17 sa2 Nitrate 1.8391 1 .8473 1.8535 1.8474 18 sa3 1.8607 1.8669 1.8754 1.8669 19 96 K2304- sa1 Potassium 1.864 1.8869 1.8848 1.8836 kclsa2 Sulphate 1 .8629 1 .8776 1 .8772 1 .8764 kclsa3 1.8853 1.9043 1.9035 1.9014 192 (continued from table M5) Date : 11/7/2003 1 1/9/2003 11/17/2003 SNO. %RH PAN Chemical No. Name 1 1 1 Licl-sal Lithium 2 sa2 Chloride 1.753 1.75 1.75 3 sa3 1.7874 1.7871 1.7871 4 45 K2co3-sal Potassium 1.7536 1.736 1.735 5 sa2 Carbonate 1.785 1.7851 1.7851 6 sa3 1 .7442 1 .7441 1.744 7 56 Mg2No3-sal Magnesium 1.7221 1.722 1.7222 8 sa2 Nitrate 1 .7602 1 .7602 1.7603 9 sa3 1.7602 1.7602 1.7604 10 77 Nacl-sal Sodium 1.7426 1.7425 1.743 1 1 $32 Chloride 1.792 1.7922 1.7923 12 533 1.7782 1.7782 1.7792 13 8400% Kcl-sal Potassium 1.7935 1.7936 1.794 14 sa2 Chroride md 15 sa3 1.8088 1.8091 1.81 16 90 K2No3-sal Potassium 1.8606 1.8595 1.8661 17 sa2 Nitrate 1.8472 1.8465 1.8535 18 333 1.8683 1.8683 1.8754 19 96 K2504- sa1 Potassium 1.8816 1.8837 1.9094 kclsa2 Sulphate 1.8774 1.8809 1.9039 kclsa3 1.903 1.9075 1.9333 193 (continued from table M5) SNO. %RH PAN Chemical No. Name We Avg We Wi Avg Wi 1 11 Licl-sa1 Lithium 0.4982 2 sa2 Chloride 0.4677 0.5016 3 sa3 . 0.5125 0.4901 0.5278 0.5092 4 45 K2C03-sa1 Potassium 0.4640 0.4875 5 $32 Carbonate 0.5090 0.5133 6 533 0.4749 0.4826 0.4778 0.4929 7 56 IM92N03-3a1 Magnesium 0.4479 0.4464 8 $32 Nitrate 0.4790 0.4774 9 sa3 0.4971 0.4747 0.4944 0.4727 10 77 Nacl-sa1 Sodium 0.4791 0.4588 11 $32 Chloride 0.5259 0.5019 12 sa3 0.5036 0.5029 0.4807 0.4805 13 8400°/o Kcl-sa1 Potassium 0.5248 0.483 14 sa2 Chroride 0.4752 15 sa3 0.5273 0.5261 0.4868 0.4817 16 90 K2No3-sa1 Potassium 0.5862 0.4879 17 sa2 Nitrate 0.5781 0.4809 18 sa3 0.6026 0.5890 0.5042 0.4910 19 96 K2$o4- sa1 Potassium 0.6324 0.4996 kclsa2 Sulphate 0.6284 0.4969 kclsa3 0.6524 0.6377 0.5133 0.5033 194 (continued from table M5) SNO. % RH PAN Chemical No. Name °/o RH Me Aw Aw/Me 1 11 Licl-sa1 Lithium 0 0 0 0 2 sa2 Chloride 3 $33 11.0000 0.0841 0.11 1.3087 4 45 K2co3-sa1 Potassium 5 sa2 Carbonate 6 $33 43.0000 0.1029 0.43 4.1782 7 56 IMgNo3-sa1 Magnesium 8 sa2 Nitrate 9 $33 53.0000 0.1309 0.53 4.0487 10 77 Nacl-sa1 Sodium 1 1 $32 Chloride 12 $33 75.0000 0.1788 0.75 4.1944 13 8400% Kcl-sa1 Potassium 14 sa2 Chroride 15 $33 83.0000 0.2301 0.83 3.6074 16 90 K2N03-sa1 Potassium 17 $32 Nitrate 18 sa3 90.0000 0.3510 0.9 2.5639 19 96 K2504- sa1 Potassium kclsaZ Sulphate kclsa3 96.0000 0.4272 0.96 2.2470 195 GAB model constants and T ,C Wm and K Values for GAB model at 30C: 0t = -13.726 B = 15.643 Y = -0.1 123 T -154.7509 C = 0.9936 Wm = 00647 K 138.4135 RMS Calculations: Table M 6. RMS calucaltions at 30°C and different %RH conditions Aw CkAw (1-kAw).. M (Gab) M (Exp) 0 0 0 0.11 15.1283 —12.8437 0.0763 0.0841 0.0932 0.0087 0.45 61.8887 -36.9326 0.1085 0.1029 -0.0544 0.0030 0.56 77.0170 -38.6759 0.1289 0.1309 0.0151 0.0002 0.77 105.8984 -33.7904 0.2029 0.1765 -0.l499 0.0225 0.84 115.5256 -29.7663 0.2513 0.2301 -0.0922 0.0085 0.9 123.7774 -25.3637 0.3160 0.3510 0.0999 0.0100 0.96 132.0292 -20.0810 0.4257 0.4272 0.0036 0.0000 0.0075 RMS 8.6861 196 APPENDIX D THERMAL INSULATION PROPERTIES CALCULATIONS OF GREEN CELL® FOAM. Table T 1. (R-Value ) calculation of GCF and EPS coolers at 50%RH and 25°C Condition 2 50%RH and 25°C Preconditioning time = 145 minutes=2.4l6 hrs Inside temperaturele =32°F Outside temperature=T2=77°F Temperature difference: 45° F Latent heat of ice: 11b of ice at 32F absorb 144btu(36.3Kcal) Area of cooler EPS=2(LD+WD=LW)=4.421ft2 Length Width Height L w D 2LD 2WD 2LW Area Area in in in 1.12 ft2 11.875 10 9.125 216.71875 182.5 237.5 636.719 4.4217 Area of cooler Green Cell C0016F=2(LD+WD=LW)=4.37ft2 Length Width Height I L W D 2LD 2WD 2LW Area I Area in in in in2 ft2 11.687 10 9.125 213.28775 182.5 233.74 629.528 4.3717 EPS Coolers wt. Of Trial wt of bucket wt. Of water wt. Of water water Time Melt Rate R- value No. and ice collected lbs ml kg lbs hr lbs/hr hr.ft2.F/Btu 7 2350 2.35 5.17 48 0.1077 12.8250 2 7 1061 1.061 2.3342 24 0.0973 14.2019 197 Green Cell cooler trial no. wt of bucket wt. Of water wt. Of water wt. Of water Time Melt Rate R- value I and ice collected I lbs ml kg lbs hr lbs/hr hr.ft2.F/Btu 1 7 2500 2.5 5.5 48 0.1 146 11.9182 2 7 l 125 1.125 2.475 24 0.1031 13.2424 Table T 2. (R-Value ) calculation. of GCF and EPS coolers at 80%RH and 30°C Condition = 80%RH and 30°C(86F) Preconditioning time = 145 minutes=2.4l6 hrs Inside temperature=Tl=32°F Outside temperature=T2=86°F Temperature difference: 54 °F Latent heat of ice: 11b of ice at 32°F absorb l44btu(36.3Kcal) Area of cooler EPS=2(LD+WD=LW)=4.421f12 Length Width Height L W D 2LD 2WD 2LW Area Area in in in in2 f8 1 1.875 10 9.125 216.71875 182.5 237.5 636.719 4.4217 Area of cooler Green Cell coole1=2(LD+WD=LW)=4.37ft2 Length Width Height L W D 2LD 2WD 2LW Area Area in in in in2 ft2 1 1.687 10 9.125 213.2878 182.5 233.74 629.528 4.3717 EPS Coolers trial no. wt of bucket wt. Of water wt. Of water wt. Of water Time Melt Rate R value and ice collected lbs ml kg lbs hr lbs/hr hr.ft2.F/Btu 1 7 1950 1.95 4.29 26 0.165 10.0455 198 Green Cell cooler Trial no. wt of bucket wt. Of water wt. Of water wt. Of water Time Melt Rate R value and ice collected lbs ml kg lbs hr lbs/hr hr.ft2.F/Btu l 7 2400 2.4 5.28 26 0.2031 7.8036 Density Calculations: Table T 3. Density calculation of l-inchand 2-inch Green Cell® foam 1 " thickness Green Cell Foam s.no Weight Weight Volume Density (g) (lb) w* L * D (lb/r13) (in’) 1 20.78 0.04577 25.2123 3.1368 2 30.98 0.06823 37.6068 3.1349 3 15.39 0.03389 19.9149 2.9405 Ave. 3.07073 2 " thickness Green Cell Foam Weight Weight Volume Density (g) (lb) w* L * D (Ib/ft3) in3 1 123.78 0.2726 141.504 3.3288 2 135.15 0.2976 149.216 3.4463 135.32 0.298 156.224 3.2961 Ave. 3.3571 Average value of 2-inch thick foam = 3.351h/ft3 Average value of 1-inch thick foam = 3.071b/ft3 Average value of l-inch thick and 2- inch thick foam = 3.211h/ft3 199 APPENDIX E PREPARATION OF SALT SOLUTION ASTM STD. E 104 Salt Solutions. Materials . Biodegradable Starch based foam (Green Cell®) ' 80 Aluminum dishes ' 3 sets of HDPE buckets, every set contains 8 HDPE buckets, maintained at different relative humidity (%RH) conditions and three different temperatures (20°C, 25°Cand 30°C). ' 8 aqueous salt solutions to create different (% RH) condition in HDPE buckets. Reagents Total ten chemicals were used to create different relative humidity conditions like Lithium Chloride, Potassium Acetate, Magnesium Chloride, Potassium Carbonate, Magnesium Nitrate, Sodium Nitrite, Sodium Chloride, Potassium Chloride, Barium Chloride, Potassium Sulfate. Reagents grade chemicals were used to prepare all standard salt solutions according to ASTM standard E104 [2]. Saturated salt solutions were prepared by using hydrated reagents. Hydrated reagents are often preferred to amorphous forms for their solvating characteristics. Equilibrium Relative humidity values (standards and actual) for selected saturated Additional reagents and Equipments I Demilitarized water: I Analytical Balance (sensitivity is i0.0001 grams) 200 I Vacuum Oven (SO-75°C and 22-25 inches Hg) I Hygrometer I 24 Pyrex container I Hot Plate I Magnetic stirrer. Preparation Method 2.1.3-a Preparation of salt solution: A quantity of the selected salt was weighed into the Pyrex container and water was added in about 2-ml increments. Each container was heated on the hot plate to maintain a constant temperature; one magnetic stirrer was inserted into the container to provide mixing, until equilibrium was reached. [2] A saturated salt solution occurs when any excess quantity of undisclosed solute is present. After preparing the salt solution, the containers were placed inside the HDPE buckets and tightly closed with a lid .One hour was given to maintain the temperature stabilization before checking the first reading of humidity by Hygrometer. The stability of the humidity conditions was checked periodically over a three weeks period. Table S-l shows the Equilibrium Relative humidity values (standards and actual) for selected saturated solutions. 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