I ITITI III ‘I TIT TI TITIIIII‘I .II‘ TI T T' ELECTRON MULTIPLI‘ER INVESTIGATIONS THESIS FOR THE DEGREE OF ELECTRICAL ENGINEER WARREN HERBERT BLESS I 9 3 9 Inlot V|rc ‘(.11u.l ,- rps.\ LEI .. no .Ivu.~uq:r. N fluid? wk {11 I; .1 1:3:(u D u ..... .IA-l¢£I.tl.L‘q.; I... ..u .1 A...» » f‘vfiLIJ. “rut v. T ELECTRON MULTIPLIER INVESTIGATIONS A Thesis Submitted To The Graduate Council of Michigan State College of Agriculture and Applied Science by Warren Herbert Bliss ~ Candidate for the Degree of Electrical Engineer June, 1939. ' .J T 7» up sum“. 3. IHESTS Electron Multinlier Investigations Table of Contents References Sheet 1 Pages of subject Matter Sheets 2 to 21 inclusive Figures Sheets A to L inclusive Photographs .; R-318 R—319 3-320 {-332 3-333 3-334 3-344 121475 References l. 2. 3. The Secondary Emission Multiplier - A New Electron Device. V. K. Zworykin, G. A. Morton, and L. Halter. Tarch 1936. Issue of Proceedings of the Institute of Padio Engineers. secondary Emission Electron multiplier. An article in the November, 1935 Issue of Electronics. Electrostatic Focussing in Secondary Emission nul— tipliers. Engineering Report TP-369, RCA Victor Div- ision, by J. Hajchman and E. L. Pike. l - Svnqps1s 1.1 - Purpose of the Investigation The investigation which is outlined in this report was carried out with the following threefold object as a guide: ~ (A) To obtain a working knovledge of light controlled, secondary emission, electron multiplier tubes. (B) To determine the practicability of vacuum tubes of this type then employed with suitable circuits and auxiliary efiuipment to generate high Speed facsimile test waveforms. (C) To consider a few possible scanner arrangements and briefly outline for reduction to practice those that are found to be suitable. ’ 1.? - General Procedure A ten stage, photoelectric type, secondary emission electron multiplier tube was obtained from the tadiotron Division at Harrison and a test "tea—Wagon" was built up to house the eeuipmcnt which included a television receiver type power pack obtained frcm the Victor Division at Gam- den and a 1500 volt rectifier. A special light source, lens system, and chopper disc assembly was constructed for supplying light to the tube. Static and dynamic characteristics were determined, the latter tests being made prircipally at 60 and 12,000 cycles per second. A few tests were made to determine the feasibility of introducing an a-c carrier frequency into the electron multiplier so that a light modulated a—c wave mould re— sult in the output. This was tried electrostatically and magnetically. The electron multiplier output was also used in a balanced modulator to modulate a 75 kc carrier. In con— nection with this a special compensating or counter emf circuit was used to improve the linearity of the modu— lator. The re-occurring phenomena generated by the Specially prepared chOpper disc was used successfully to test facsimile terminal facilities at keying speeds up to 12,000 cycles per second. 2. _ 3 _ 1.3 - General Statement of Findings On the basis of information obtained to date the electron multiplier has a very definite promise of providing at least one scheme for satisfactorily scanning subject matter at "page a minute" speed. The apDaratus arrangement to be de— scribed provides an extremely flexible tool for use in the investigation of high Speed facsimile terminal and radio cir- cuit requirements. Recommendations Experience with the electron multiplier test assembly de— scribed in this report indicates that it can be successfully em— ployed to generate accurately controlled high speed facsimile test phenomena. It is accordingly recommended for studying terminal and radio circuit requirements. It is also recommended that the study of the general per- formance characteristics of various electron multiplier modifica— tions be continued in cooperation with the Victor and Radiotron divisions of RCA—Manufacturing. Also, as time permits, that detailed consideration be given the following: (a) Introduction of carrier ac into the multiplier by the electrostatic method. (b) Determination of the minimum number of multiplier stages or minimum total voltage necessary to give sufficient output for scanner applications. (0) Further deveIOpment of a suitable modulator, probably a balanced type. (d) If theoretical considerations and preliminary experimental work indicate the desirability, the construction of a high speed scanner using a suitable electron multiplier tube as a pick—up unit. Detailed Discussion of Investigation 3.1 - Statement of Problem For the study of terminal and radio circuit reouirements for the successful handling and transmission of high speed facsimile signals it was desirable to have a test apparatus or device which would produce such signals or waveforms of voltage and current. Ordinary vacuum tube oscillators do not readily produce these and hig~ speed scanners were still in the process of deveIOpment. 3.2 - - 4 _ Furthermore, there was still the desirability of determining a suitable scanner to be used in a facsimile system capable of handling a letter size sheet per minute. In present speeds of facsimile operation there is barely enough output from the photocell to operate circuits of minimum acceptability. Higher speed operation requires improved reaponse, especially a linear frequency characteristic covering a wider band. Higher outputs are also desirable, since, with these, some of the well known types of modulators could be controlled directly. The photoelectric type, secondary emission electron multi— plier appeared to be a unit which would supply hoth of the needs outlined above. Hence, it was decided to make a preliminary in— vestigation of the characteristics and some possible applications of multipliers. Resume of Electron Multiplier Theory The construction,.theory and operation of secondary emission multipliers has been described at length in Reference 1. A brief treatment will be given here to familiarize the reader with the functioning of the magnetic, photoelectric type. Fig. l of Sheet A shows the arrangement of electrodes and resistors inside the tube and also the usual external connections for a 10 stage experimental tube. The electrodes are divided into two general groups —————— accelerating plates and emitters. Electrodes b, d, f, h, j, l, n, p, r and t belong to the former group and a, c, e, g, i, k, m, o, q and s to the latter. v is the collector and u, the screen. In the tube used in this investigation the first 6 accelerating electrodes were made of screen so that light could be focused on any one of the first 6 emitters. The multiplying action in the tube is a result of the ratio of secondary emission electrons to bombarding electrons on the emitters being greater than unity. Light, falling on the first emitter a, releases electrons by photoemission (the emitters are capable of photoelectric emission as well as secondary emission). These electrons are attracted by and accelerated toward electrode b which is at a higher potential than a. Except for the presence of a magnetic field whose lines of force are at right angles to the plane of the sketch in Fig. 1, sheet A, the electrons would go to plate b. However, the combined influence of the electro- static and magnetic fields causes the electron path to be curved as shown in the sketch so that the electrons arrive at plate c which is at the same potential as b. The electron velocity at this bombarding point is sufficient to cause appreciable second- ary emission. A ratio of secondary electrons to primary electrons of 3 per stage can readily be obtained in a 10 stage multiplier. The increased number of electrons emitted by plate c is acted on by the next accelerating electrode and the magnetic field and then bombards plate 3. In this manner the electron streams are amplified as they pass down the tube until the last plate v collects the final emission from s. The distribution of voltage on the numerous electrodes is accomplished by means of a tapped resistance bleeder. To avoid having too many terminals on the tube the bleeder resistors for the first few stages are Inounted inside the tube envelope. The output current may be passed through a resistor PL where an emf proportional to the light will be develOped. 3.3 - The Physical Setup 3.31 - General Fig. l of Photograph P-319 shows the general arrange- ment of the electron multiplier test setup. This shows the top compartment of the "tea-wagon" with the light source and chOpper disc assembly. This compartment is 26 inches wide by 17 inches deep by 15 inches high. The front and top, which are on hinges so they may be turned up and back out of the way, are equipped with interlocking switches so that the power supplies (1500 volts and 6300 volts) cannot be turned tn while the compartment is open. The tOp, front and right hand and are made of transparent material so that meters may be observed from outside. The bleeder or voltage divider resistor bank is mounted in the back of the COMpartment and the output meter and inner tube compartment, toward the front. Fig. 2 of Photograph D~320 is an inside view of the inner tube compartment taken from above. The field magnet is shown pulled back to bring the tube into view. A rotatable base is controlled by an external knob so that the tube may be turned about its axis to bring it into proper relation with the magnetic field. Slots through both compartments provide an unobstructed path for the light beam. PhotOgraph R-344 and Fig. l'of Photograph P—32O show the light source assembly. This unit was made to simulate the reflected light produced in an actual scanner. It was designed to comply with this in three respects: 3.32 - -6- lst, same aperture distortion, 2nd, same light quantity, and 3rd, same top frequency of light fluctuation for page a minute speed. The assembly consists of a lamp house, 10 volt lamp, a lens barrel, and a motor driven chopper disc. Details of Light Source Assembly. Fig. 2 of Sheet A gives the details of the Optical system. The light is supplied by a 50 watt, 10 volt lamp 1 which is operated at 8.5 volts. The first unit in the lens barrel is a condenser lens 2. From this the light passes through two screens 3 and A. The first is one of fixed density which was chosen so that the light output of the syssem felling an plate 11 would be the same as that reflected from a conventional scanner drum fir ' white subject matter. This value is about 6.4 x 10- lumen. Screen 4 is a stepped, density wedge slide, the tOp of which may be seen in Photograph R-344 projecting upward to the right of the lamp house. The next important part of the optical system is the aperture 5. Two of these were used; the first one was 0.025 inches square and the second, 0.012 inches high by 0.025 inches long. These values, as will be explained later gave the desired aperture distortion. Lens 6 focuses the image of aperture 5 on the chopper disc 8. A mask 7, having a small round hole through its center, cuts out most of the stray light arriving at this section. Lens 10 picks up the light as it comes through the chOpper disc and brings it to a 5 millimeter spot on the photoelectric cathode ll of the tube which is to re- ceive the light. A close inspection of Fig. 1, Photograph R—320 reveals the details of the chopper disc which is driven at 1800 RPM by a 60 cycle, synchronous motor. Two alternate 90 degree segments of the disc are solid. The other two alternate 90 degree segments are divided radially into six different bands.‘ The outer or first band is cut away so that when this position is used 60 cycles per second square wave chOpping is done. The second band has 100 teeth and 100 slots, each 0.032 inches wide, in each of the two 90 degree segments. This band, then, produces 12,000 cycles per second chapping. The next four bands produce, reSpecte ively, A impulses, 3 impulses, 2 impulses, and 1 impulse of 12,000 cycles. The disc drive motor is mounted on a - 7 _ sliding base so that any one of the six bands may be brought into the light beam at the proper point. Chomper Frequency Considerations and Aperture Distortion For a 10 inch page per minute scanning the Screw Advance 3 .12 3 0.1667 inches/sec. 60 For standard line advance of 120 lines ner inch the Screw Advance = 0.1667 x 120 = 20 lines/sec. For a standard drum circumference of 9.22 inches the Linear Scanning Speed = 20 x 9.22 = 184.4 inches/sec. The stems and bars of letters of 8 point type are 0.0082 inches wide. Taxing twice this value or 0.0164 inches as the length of a cycle in scanning such letters, the following is obtained. Maximum Fundsmental Scanning Frequency for Page a Minute Speed = l84.4/0.0164 = 11,244 cycl s/second. Hence, the chOpner disc was designed to simulate 12,000 cycle scanning, which is a slightly greater requirement than that actually expected. In the standard AA-914 scanner the light sDot as it strikes the drum surface is 0.006 inches by 0.008 inches. The first dimension is that measured parallel to the direction of motion of the drum surface at the scanning point. Hence, the period of aperture distortion in scanning a letter bar cycle ( = 0.0164 inches) is given as Aperture distortion 3 0.006 = 0.366 cycle 0.0164 2 0.366 x l 3 32.5 x 10'6 sec. 32.5 microseconds for page a minute scanning. In designing the chOpper disc a diameter of 8 inches was selected. Too large a disc would require a large motor and too small a disc would require teeth and slots too small to be made accurately. with the 8 inch disc the teeth were made witha 1/32 inch cutter and spaced about 1/16 inch apart (center to center). This made the finished teeth and slots each practically 0.032 inches wide. For the same aperture distortion as discussed above the light spot should have a Width = 0.366 x l = 0.0228 inch 16 The aperture 5 (Fig. 2, sheet A) was actually made 0.025 inches souare 1.hich gave slightly more distortion. The oscillograms shown on Photograph sheet R—332 were made with this aperture. Since the duration of the flat top Of the wave was very short another aperture having a width Of 0.012 inch was made. The oscillographic results of this are shown on Photogra1h sheet 3-333. 3.4 - Static Characteristics Figs. 1 and 2 on sheet B are sketches Of the circuits used injeternining some Of the static characteristics of the electron multiplier and on sheets C and D are the curves resulting from these tests. The double, heavy voltage divider system shown in the circuit diagrams was used to ins e sood voltage regulation at all the multiplier terminals. Practically all the tests were made with a total potential of 1500 volts which was diviied into 130 volts per stage and 200 volts for the collector or anode. With this condition and zero resistance in the anode circuit the data for the resonance and linearity characteristics shown on sheet C were taken. Fig. 1 shows the relationship betwe een the anode current and the magnetic field strength for the major resonance peak n. This curve is similar to one shown in reference 1 and shows the nece:3sitv Of holding the field coil current constant. It was observed that operation of the tube in either side of the resonance pea: caused appreciable noise in the output res ulting from small irregularities in the high voltage or field supplies. The most stable Operation, as well as the maximum output, was Obtained when the conditions were 8 dch that the tube "as performing at the tOp of the resznance hump. The amount of light used in this test was about 5 x 10 lumen. _ 9 _ Fig. 2 of sheet 0 is a linearity check on the multiplier for small quantities of light. A light density wedge was cali- brated by means of a standard type 913 photocell with a compar— atively large amount of light and then 'he wedge was used to check the multiplier with about 5 x 10- lumen maximun. No data was taken for large anounts of light since the saturation point was believed to be well above one millianpere of output current. Figs. 1 and 2 on sheets B and D show the test circuits and results of variation of load resistance. Fig. l on each sheet is the case for normal operation with the load resistor in the anode circuit. with this condition the output terminal at ground potential is the plus lead. The circuit was also arranged as in Fig. 2, sheet B, so that output voltage of reversed polarity with respect to ground could be obtained. In this case the terminal at ground potential is the negative lead. Both of these schemes were tried because either polarity, with respect to ground, mar be desirable depending on the type of modulation to be produced. It should be noted that there may be objections to the second scheme since the variation in IR drop across . the load resistor alters the potential of the last emitter and the accelerating electrode connected to it. However, the curves for output voltage are similar in shape, and in practice the load resistance may be kept low enough to limit the output to a few volts so that this alteration of electrode potentials may not be Objectionable. The two tests discussed above were conducted with 6.4 x 10'4 lumen of light, which value, as mentioned previously, is equivalent to that reflected from white subject matter on a standard facsimile drum. This va ue was determined by measuring the current in a type 918 phototube when receiving the reflected scanner light. The light from the light chopper lens system was then directed into the same cell and a light screen selected to pronuce the same cell current. It was assumed that discrepancies due to color differences in the two sources could be neglected. The numerical value given above results from the rated sensitivity of a 918 cell (110 microamp./ lumen) and the measured cell current (0.07 microamps.) -3-5 - Dynamic Characteristics (Experimental) Photographs R-332 and R—333 are the results of a series 01? tests on the electron multiplier when operating with "chOpped" itight. The circuit of Fig. 1, sheet B, was used to Obtain all of tilese. For the oscillograms en R—332 the aperture distortion was 322 microseconds for the 60 and 12,000 cycle tracings and 43 micro— Senzonds for the 8000 cycles while the quantity of light for all W843 about 10"3 lumen. For those on R-333 the aperture distortion was 16 microseconds and the uuantity of light, 6.4 x 10-4 lumen. Thrase two groups of oscillograms were obtained by contact ex— lasc screen of the RCA type THV-l22-D L) 3x>£fiure prints on the g °S<3fillosc0pe, whose vertical sensitivity was 90 volts per inch. -10... In considering sheet H—332 the effect of load resistance and capacitance on the wave form is not very evident except for the 60 cycle souare waves. The influence of these factors on magnitude is quite prominent, however. Referring to Figs. 1 and 5 or to Figs. 2 and 6, the output voltage is seen to be preportional to the load resistance as would be expected. In Fig. 5 the output voltage oeaks are 70 volts. A comparison of Figs. 2 and 4 shows a decrease in magnitude due to the current shunting effect of a small condenser in parallel with the load resistance. The aperture distortion was so great for these cases that the waves appear to be almost sinusoidal. The 8000 cycle oscillograms were obtained by driving the chopper motor from a 40 cycle mechanical fork supply. The ten— dency for flat tOp on the waves is evident in Fig. 1. The theor- etical duration of flat top in this case is 1/8 of a cycle. In spite of the efforts to reduce the stray capacitance to an ab- solute minimum the corners of the waves are still slightly rounded. Fig. 7 shows the quality of wave form for 60 cycle square wave with an aperture distortion of 32 microseconds. This wave is perfect for most practical purposes. Fig. 8 shows that the shunt or stray capacitance can be as great as 3.005 mfd. before this waveform is altered appreciably. I ‘ The waveforms on sheet R-333 give a better indication of the dynamic performance of the multiplier. With the aperture distortion reduced to 16 microseconds the flat—tOpped nature of the waves is very pronounced. Figs. 9, 11 and 13 show the effect of varying the load resistance; With values of 100,000 ohms or higher the flat top is distorted. For a 50,000 ohm load the waveform is good and the peak value of voltage is 22 volts; this is from 6.4 x 10‘4 lumen of light. Reducing the load resistance below 50,000 ohms improves the wave shape slightly but decreases the output voltage directly. Figs. 10, 12 and 14 show the influence of shunt capacitance. The first and last of these were taken with a load circuit time constant of 10 microseconds which distorts the waveshape appre— ciably. The wave of Fig. 12, which was made with a time constant of 5 microseconds, might be regarded as the limit of allowable distortion but even in this case there is a time lag which does not show up in the oscillogram. See section 3.6 of this report for explanation of this lag. Figs. 9 and 15 were made with identical circuit conditions but the latter was produced with the light juantity reduced considerably. This test was carried out to show that the waveform (except for change in magnitude) depends solely on the circuit constants. A close examination of these oscillograms will show that this is true. The magnitudes are different but the forms are the same. 3.6 - Fig. 16 was made to show the effect of light saturation on the output waveform. The peak value of current in this case was about 5 milliamperes and the light, several times normal. Dynamic Characteristics (lheoreticall The response of the load circuit of the multiplier to the output current wave caused by incident light fluctuation can readily be determined mathematically as follows: Except for the case where the load circuit contains series inductance the output current from an electron multiplier or a photocell can.be expected to follow the incident light fluctuation almost precisely. This is true only as long as these devices have sufficient anode potential to be well above the saturation point. The output current is then independent of the applied voltage. It is the purpose of this treatment to show how much the voltage across the load resistance deviates from following the incident light variations when leakage or stray shunt capacitance exists across this load resistance. Two cases will be considered: First, the response to a single rectangular impulse, and second, the reSponse to a single synmetrical trapezoidal impulse. Case L Fig. 1, sheet F, shows the circuit and notation that are to be used. For Case I i = f(t) will be defined by /':f(C)=0 fir 1(0) i:f(t)31 for Ot,. Applying Kirchhoff's First Law to the Circuit gives fear-1,21. Applying Kirchhoff's Second Law gives . _ I ' R ’3 “ET/)6 (It. (3) Combining (2) and (3) produces ' . . l , I=IC+RC/’c dr- (4) IHeaviside's operational notation and method may readily be 8tpplied to (4). - 12 - (”Fa—6%?“ ‘ (5) . / P_ or Ic=(P+§-Lc—)I7 The solution of (6) is . t/ .. ‘ RC Since the load voltage, eL, is desired, it is obtained thus, 6L: 3’5 =R(I-I;) =RI(/~ 6‘”? (a) This is a well recognized form. It is similar to the ex- pression for the rise in current in an BL circuit when unit function voltage is applied. Fig. 1, sheet E, shows the rec— tangular impulse as plotted for the case of R = 50,000 ohms, C I 100 mmfd. and I = 5 x 10’4 amp., up to the point where t = t1 = 30 microseconds. ' Beyond where t - t1 1 - o and iC = -i . If the variable t is now measured from t1 as a new zero point the condenser dis- charges through the resistor according to . ..C IR: Inc? ”'3 (9) where Ir is the initial value of the discharge current. The load voltage in this case is 8L: RI, 5%" (10) This has also been plotted on the same graph. The complete curve shows the characteristic "rounding of the corner" effect that is frequently noticed when square wave is applied to amplifiers, filters and other circuits. The smaller the value of BC (the time constant), the more nearly the response approaches the actual applied waveform. Case II In facsimile scanning the light variation is never a true rectangular waveform due to aperture distortion. The theoretical I not} Wen-“4.5 _ 13 - variation simulates a trapezoid as illustrated in Fig. 2 of sheet E. For this case i = f(t) may be defined by a i: (717:0 for t< a, i: {[19:52 for 0>RC. (21) The load voltage in practical cases soon lags the ideal wave by an amount equal to the time constant of the load circuit. Period B (z. < t < 12) During this interval 1 - f(t) a I. Using i and iC again as the current symbols and measuring time from t = t1 as the new zero point, the application of Kirchhoff's laws gives and Riflzfcf-EI-fl; dt, (23) where Ec is the initial condenser voltage. Solving (22) and (23) gives ° . ~VRc Q=IE’ , ‘ Wu in which I '=: (I- £57 From this . . c “(/86 8‘: RIR:R(I-Ic)=RI‘RIE , (25) This function is also plotted on the graph'between the points marked t and t . For the numerical values used eL practically reaches the steady state value at the latter time, t2. Period C (t2 < t4 :3) Measuring t from t? as a new zero our fundamental equations become grézI-KZ (%) INN v. :3 “4...“. . -16- and RiflzEc'I'El—flé JZ‘. (2'7) ’;=(P*;%)[2I~%)IK€]7° (3:) Using the Superposition Theorem again gives 4; = (I‘ §¢_)E-C/Rc_/yé~(t~A)/Rcd A (29) a or I;=(I- %—)€VR€ KRC(I~ «SJ/"‘7. From these (30) Then eLsRI +KR2c~th +(Ec-RI~ MOE?“ (31) The plot of this curve between t and t on the graph shows a lag on the voltage decay similar to that on the build-up. This, of course, is what was anticipated. Period D (t >t3) Equation (10) will apply in this case .t/Rc 6":56 (32) t being measured from t as a new zero and E0 is the value of eL oat t3 from equation (31;. This completes the theoretical reSponse curve of the load voltage. Two facts have been brought out by the above considerations. I. The original wave is changed in form by the presence of shunt capacitance. II. The response for a trapezoidal wave lags the original wave by an amount which Quickly approaches the time constant of the circuit as a limit. -17.. The oscil lograms of Photograph 3—333 check the above theory in respec ct to the first fact but do not shoe the lag very well. A Specia he t techni«_ue would be re uired f'or this The same numer- ical values of the circuit factors were used to cbt1§n +he oscillo— gr-m of Fig. 12, sheet R-333, as were sed for the theoretical case of Fig. 2, sheet E. The shape of these two curves is the same. 3.7 .Modulation Schenes In facsimile systems for picture transmission via radio the light fluctuation picked uo by the scanner is usually used to modulate an ac carrier. Several schemes were tried in connection with the electron multiplier as exnlained bel w. 3.71 - Carrier Annlied Electrostatically to the Electron hultiolier In order to determine the feasibility of introducing the carrier emf in series with one of the multiplier electrodes the static characteristic shown on sheet G was obtained by means of the circuit of Ei_g. 2, sheet F. The potential f nllmber 3 ele ectrode (this is actually the joint connection of emitter o and accelerating electrode n, see Fig. l, shee A) was varied over a wide range and the correswonding var— iation in load current noted. If the electrode is onerated at a dc potential of + 40 volts with respect to the preceding electrode, a cabrier emf having a peak value of 60 volts may be introduced. The output current should then.vary directly with this carrier since the curve is linear over the range covered. This scheme was tried with a 60 cycle s uare nave li;' ht variation and an 310 cycle carrier. Fir. l on Photograph —334 is the resulting oscillogram of the output. This os— cillogram was reproduced from a nencil tracing. The modula- tion enveloge has two serious disadvantages. First, 100 per- cent modulation without distortion was impossible, and second the envelooe has a varia.ble dc component. There is no system knovn to the writer which will separs te out the dc component of this type of 1ave iithout distorting the have envelOpe. Unless his fundamental difficulty is over- come the electrostatic methoc of introdlcin ng the carrier does not appear promising. 3.72 — Carrier Aeolied Ha.oet1c 11" to the Electron EulH ilisr An attemp, was made to introduce the carrier by nodu— lating the magnet'c ii eLl of the multidlier. The results were less pron Tsi.g th“.u for the electrostatic method. 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Carrier ~' Input 1 Winn ...-...... ...“ .. . ‘3' “le11§q414§1:11§<1l4§H 3% ‘ 4 .I .1 14.1. 4| 1} nl E 14‘ . ‘ ‘ \ lunar n rfiéuxbflrks .. .L. - b. artisa; n... «.1 ..m r.» f: .o mwhm 91229 :2 - "4 z m‘~ m9m1*1'-H'JNE'V*'W '— I ~ gm“. ‘0 F19. L III-I'llwfluh'.“ ..m .Ilv i. n . ‘ .1. I. Fig. I F =8000v- Fig.2 172/2000" R = 25000n C . 0 3'25000» C '0 ;- - ‘ ..-.“- Fig.3 Faaooo - Fe). 4 ' Fa Izooo .. R’ZJOOOA 6:0.000‘5/14f "'25000“ 020.0005uf A Fig.5 F-aoao - Fig.6 F . 12000 *~ R =sooooa c to R =Soooo~ c :0 — — - —. D -’ - - d - n9. 7 Peso .. Fig.3 Few-a R250000A C'O R’500004‘- . C-‘QOOJLJ mama/v mummm OUTPUT WAVEFORMS R9223; A Fig.9 R amo, 0004- 6:0 Fig.“ 0,000-"- 12:0 641. w, Fly. 13 R-2.£000-‘- C = 0 .. : \\\\\“ w- - F19. I: R=I04000v~ (“=0 Lyhr Reduced ELECTRON MULTIPL/ER L:— Fig. [0 R2 ’00, 000‘“ 0: 0.000 Lat A..- R=n5'0,000“- 6:0.000M1S W F13. I4 R=50.000"" ——-.—- ... sz9./6 R=I6,000- 0:0 Lighr Increased OUTPUT WA VEFORMS 95226. R-333 ELECTRON MU! T/PL/ER MODULA TED ’ WA V5 F OR M8 W F {9. I 60 "‘ Chopper 8/0m Carrier “fl wf H n}: W Fig.2 [2,000m Chopper 7.5 KC. Carrier ‘1 ‘ Fig. 3 ‘60 " Chapper .3240M Carrier 95225.. R-33‘fi . . 1. . . . A V _ . ... , A K, . ...».t. P. .r. . I . I v ”2: .c» .l .. . .. ‘ ‘ ... . u : v Hi? MICHIGAN STATE UNIVER ITY l n H i’um ,Ililjmfimn'“ 3 1193 03058 1