array e subpack i dynamic analysis #80...19d random vibration spectrum (lunar descent), xmtr...

NO. RI!V. NO.

ATM 989 Array E Subpack I Dynamic Analysis

PAGE OF

DATE

This ATM presents the results of the dynamic analyses performed on Array E, Subpack-1 for both the LSG and the PSE versions.

5/24/71

Prepared by:;/1. .. ..$.~ G. B. Min

kll~ K. H. Wadleigh

Approved by: ~~ J. Maszatlcs

Array E Subpack I Dynamic Analysis

CONTENTS

LIST OF ABBREVIATIONS

LIST OF TABLES

LIST OF FIGURES

SECTION:

1. 0 INTRODUCTION AND SUMMARY

2. 0 ANALYSIS MODELS

2. 1 Stiffness Matrix 2. 2 Mass Matrix 2. 3 Forcing Matrices and Input Levels

3. 0 COMPUTED ACCELERATION RESPONSES

4. 0 DYNAMIC LOADS

5. 0 REFERENCES

6. 0 APPENDIX

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Page

i

ii

iii

1

2

3 4 4

5

9

11

119

LMS

LSG

LSP

PSE

L&B

L. D.

EASE

RMS

cjs

CSE

GEO

ANT

SP

PDM

CMD

DATA/PRO. D/P, DA/PR

C/D, COM/DEC

DIPL

SW

ELEC

XMTR

.......

Array E Subpack I Dynamic Analysis ATM 989

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I..IST OF ABBREVIATIONS

Lunar Mass Spectrometer

Lunar Surface Gravimeter

Lunar Surface Profilometer

Passive Seismic Experiment

Launch and Boost

Lunar Descent

Elastic Analysis for Structural Engineering (Digital Computer Program)

Root mean square

Central Station

Central Station Electronics

Geophone

Antenna

Subpackage

Power Dissipation Module

Command

Data Processor

Command Decoder

Diplexer

Switch

Electronics

Transmitter

NO.


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LIST OF TABLES

TABLE DESCRIPTION PAGE

1 ALSEP Array E Weight Estimate 12 2 ALSEP Array E Central Station Assembly Detailed 13

Weight Breakdown (Estimate) 13 3 Generalized Coordinates (Refer to Figures 1 and 2) 14 4a Subsystem Coordinates Array E SP-1 (LSG Version) 16 4b Subsystem Coordinates Array E SP-1 (PSE Version) 17 5 Natural Frequencies and Responding Motions 18 6 Array E SP-1 Vibration Analysis Results (LSG Version) 19 7 Array E SP-1 Vibration Analysis Results (PSE Version) 20 8 Sine Loads and Deflections @ 54 Hz 21 9 Random Loads and Deflections (LSG Version) 22

10 Comparison of L&B Dynamic Loads with Static Design Loads 23


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LIST OF FIGURES

FIGURE DESCRIPTIONS PAGE

1 la lb 2a 2b 3 4 5 6 7 8 9

10 11 12a 12b 12c, 12d

13a 13b 13c 13d

14a 14b 14c 14d

15a 15b 15c 15d 16 17 18

Array E/Subpack 1, Complete Assembly Array E/Subpack 1, Sunshield Equipment (LSG Version) Array E/Subpack 1, Thermal Plate (LSG Version) Array E/Subpack 1, Sunshield Equipment (PSE Version) Array E/Subpack 1, Thermal Plate (PSE Version) LSG Equipment LMS Equipment LSP Equipment PSE Equipment Computer Programs and Assumptions Subsystem Stiffness Matrix (LSG Version) Subsystem Stiffness Matrix (PSE Version) Sinusoidal Input L&B Array E SP-1 Random Vibration Specification Levels Transmissibility, LMS X-Response u2/X Input Sine Response, LMS X-Response Uz/X-Input

c)'~ Random Vibration Spectrum, LMS X-Response U2, L&B Random Vibration Spectrum, Lunar Descent, LMS X-Response Uz Transmissibility, Location 3 X-Response/X-Input Sine Response, Location 3 X-Response/X-Input Random Vibration Spectrum, Location 3 X-Response, L&B Random Vibration Spectrum (Lunar Descent), Location 3 X-Response Transmissibility, Location 6 X-Response/X-Input Sine Response,. Location 6 X-Response/X-Input Random Vibration Spectrum, Location 6 X-Response, L&B Random Vibration Spectrum (Lunar Descent), Location 6 X-Response Transmissibility, LSP X-Response U4/X-Input Sine .Response, LSP X-Response U4/X-Input Random Vibration Spectrum, LSP X-Response U4, L&B Random Vibration Spectrum, LSP X-Response U4, L. D. Random Vibration Spectrum, Location 13 X-Response, L&B Random Vibration Spectrum, Location 14 X-Response, L&B Random Vibration Spectrum, Locatio·n 19 X-Response, L&B

24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39

40/41

42 43 44 45

46 47 48 49

50 51 52 53 54 55 56 57

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LIST OF FIGURES (CONT.)

FIGURE DESCRIPTION PAGE

19a Transmissibility, XMTR X-Response/X-Input 58 19b Sine Response, XMTR X -Response/X-Input 59 19c Random Vibration Spectrum, XMTR X-Response, L&B 60 19d Random Vibration Spectrum (Lunar Descent), XMTR

X-Response 61 20a Transmissibility, LSG X-Response @C. G. /X-Input 62 20b Sine Response, LSG X-Response @C. G. /X-Input 63 20c Random Vibration Spectrum, LSG X-Response @ C. G., L&B 64 2la Transmissibility, LSG Y -Response @C. G. /Y -Input 65 21 b Sine Response, LSG Y -Response @ C. G. /Y -Input 66 21c Random Vibration Spectrum, LSG Y -Response @C. G., L&B 67 22a Transmissibility, LSG Z-Response@ C. G. /Z and X-Input 68 22b Sine Response, LSG Z-Response@ C. G. /Z and X-Input 69 22c Random Vibration Spectrum, LSG Z-Response@ C. G./

Z and X-Input, L&B t.: 70 23a Transmissibility, LSG X-Response @Isolator U3/

X-Input 71 23b Sine Response, LSG X-Response @Isolator U3/

X-Input 72 23c Random Vibration Spectrum, LSG X-Response @

Isolator u3, L&B 73 23d Random Vibration Spectrum (Lunar Descent), LSG

X-Response @Isolator U3 74 24a Transmissibility, LSG Y -Response@ Isolator/Y -Input 75 24b Sine Response, LSG Y -Response @ Isolator/Y -Input 76 24c Random Vibration Spectrum, LSG Y -Response @

Isolator, L&B ~ 77 24d Random Vibration Spectrum (Lunar Descent), LSG

Y -Response @Isolator 78 25a Transmissibility, LSG Z-Response@ Isolator/Z-Input 79 25b Sine Response, LSG Z-Response@ Isolator/Z-Input 80 25c Random Vibration Spectrum, LSG Z-Response@

Isolator, L&B : 81 25d Random Vibration Spectrum (Luna.r Descent), LSG

Z-Response@ Isolator 82

FIGURE

26a 26b 26c 26d

27a 27b 27c, c:.~ 27d

28a 28b, b~~ 28c, c~r:: 28d

29a 29b 29c, c* 29d

30a 30b 30c 30d

3la

3lb 3Ic

3ld

32a 32b 32c 32d


LIST OF FIGURES (CONT.)

DESCRIPTION

Transmissibility, LSP Z -Response/Z -Input Sine Response, LSP Z -Response/Z -Input Random Vibration Spectrum, LSP Z -Response, L&B Random Vibration Spectrum (Lunar Descent), LSP Z-Response Transmissibility, LMS Y -Response/Y -Input Sine Response, LMS Y -Response/Y -Input Random Vibration Spectrum, LMS Y -Response, L&B Random Vibration Spectrum (Lunar Descent), LMS Y -Response Transmissibility, LMS Z -Response W 2/Z -Input Sine Response, LMS Z-Response W~/Z-Input Random Vibration Spectrum, LMS /Z-Response Wz, L&B Random Vibration Spectrum (Lunar Descent), LMS Z/Response Wz

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PAGE

83 84 85

86 87 88

89/90

9I 92

93/94 95/96

97 98 99

Transmissibility, LMS Z-Response WI, W3/Z-Input Sine Response, LMS Z-Response WI, W3/Z-Input Random Vibration Spectrum, LMS Z-Response WI, W3, Random Vibration Spectrum, (Lunar Descent), LMS Z-Response W1, W3

L&B 100/101

Transmissibility, LSP Y -Response V z/Y -Input Sine Response, LSP Y -Response V z/Y -Input Random Vibration Spectrum, LSP Y -Response Vz, L&B Random Vibration Spectrum, (Lunar Descent) LSP Y -Response Vz Transmissibility (PSE), PSE X-Response U II X-Input Sine Response (PSF,), PSE X-Response U1/X-Input Random Vibration Spectrum (PSE), PSE X-Response U 1/X-Input, L&B 1 1 Random Vibration Spectrum (Lunar Descent; PSE), PSE X-Response U I Transmissibility (PSE), PSE Y -Response V 1/Y -Input Sine Response (PSE), PSE Y -Response VI/Y -Input Random Vibration Spectrum (PSE), PSE Y -Response V 1, Random Vibration Spectrum (Lunar Descent, PSE), PSE Y -Response VI

L&B

102 103 104 105

106

107 108

109

llO Ill 112 113

114

FIGURE

33a 33b 33c 33d

A-1 A-2 A-3 A-4 A-5

A-6 A-7

A-8


LIST OF FIGURES (CONT. )

DESCRIPTION

Transmissibility (PSE), PSE Z -Response W 1/Z -Input Sine Response (PSE), PSE Z -Response W 1/Z -Input Random Vibration Spectrum (PSE), PSE Z -Response W 1' Random Vibration Spectrum (Lunar Descent), PSE), PSE Z -Response W 1 The Transformation Matrix [B) {LSG Version) The Subsystem Stiffness Matrix [KJ (LSG Version) The Transformation Matrix [B) (PS EVersion) The Unsynthesized Stiffness Matrix [K] (PSE Version) The Transformation Matrix Relat~d to C. G. [C) (LSG Version) The Subsystem Mass Matrix [Mp] (LSG Version) The Transformation Matrix Related to C. G. [CJ (PSE Version) The Subsystem Mass Matrix (PSE Version)

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PAGE

115 116

L&B 117

118 120 121 122 123

; 124 125

126 127

Array E Subpack I Dynamic Analysis I ATM_982

PAGE 1 Oil"

DATE 5/24/71

l. 0 INTRODUCTION AND SUMMARY

This A TM presents the results of the dynamic analyses performed on two different versions of ALSEP Array E - Subpack I. One version contained the Lunar Surface Gravimeter ( LSG) experiment, among others, while the other version contained the Passive Seismic Experiment (PSE) in place of the LSG.

The analysis was undertaken to obtain an early estimate of the ex-periment dynamic environments and dynamic loads in order to compare these with previous Subpack I arrays. While the previous SP-1 array basic structures were similar to Array E, the experiments involved were quite

·different. Thus it would be expected that the Array E SP-1 vibration levels would be similar to previous arrays but would differ in detail for the same ALSEP vibration environment from the LM. However, the random vibra-tion from the LM was also increased somewhat, and these effects are ac-counted for in the analysis.

Dynamic analysis of the LSG revealed internal resonances which could best be avoided by mounting the experiment on shock/vibration isolators. Such isolators are included in the mathematical model of the subpackage used in this analysis. Details of the models associated with the LMS given in this report are for the arrangement without the rubber grommets.

The LSP geophone package is considered hard mounted to the brackets for this analysis, although this is only an approximation. Part of the package is suspended in foam in the direction perpendicular to the plate. Thus the calculated LSP results are somewhat severe.

The analysis models and modeling techniques are given with a brief description of the computer program inp·llts. This is followed by the computed results such as the nat1,1ral mode frequer,cies and the plotted output responses. Finally, the subject of dynamic loads is discussed and some comparisons are made with the 20g 11quasi-steady-state 11 load factor assumed for design pur-poses.

All tables have been grouped together and all figures have likewise been grouped together to facilitate the location of the data.

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In general the computed responses agree reasonably well with com-parable previous Subpack-I measured results.

2. 0 ANALYSIS MODELS

The system mass properties used for the analysis were taken from Reference 1 and are repeated in Tables 1 and 2. The experiment packages were regarded as rectangular or cylindrical masses of the proper dim-ensions and weight but with assumed uniform mass density. The masses of the sunshield and thermal plates were distributed throughout the system. The thermal plate electronics masses were concentrated near their c. g. locations and assumed to have negligible height.

The complete assembly is shown in Figure 1, and the arrangement of the packages on the plates is shown in Figure la for the sunshield components and in Figure 1b for the thermal plate components.

In the alternate arrangement subsystem packages are the same except that the PSE is substituted for the LSG a:nd one more package is included on the thermal plate for the PSE electronics. These arrangements are shown in Figures 2a and 2b for the sunshield and thermal respectively.

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DATI! 5/24/71

The mass and dimensional characteristics of the major sunshield components are shown in Figures 3-6 for the LSG, LMS, LSP and PSE packages.

Allowing all degrees of freedom to the experiment packages but X-direction only degrees of freedom to the thermal plate packages results in a 32 D. 0. F. system for the LSG version and a 30 D. 0. F. system for the PSE version. These degrees of freedom are listed in Table 3 and are the generalized. coordinates of the two versions.

Figure 7 gives a listing of the computer programs used in the pre-sent analyses and a listing of some of the assumptions involved.

2. 1 Stiffness Matrix

The stiffness matrix for the generalized coordinate system was evolved from the element stiffness matrices by the transformation

[k) = [B) T [K) [ B) q

( l )

where the matrix [B) is the. matrix relating the subsystem coordinates to -·the generalized coordinates,'' i.e.,

{S} = [B) {q}

the matrix { S} elements are listed in Table 4a for the LSG version and in Table 4b for the PSE version.

(2)

The matrix [ K] is made up of subsystem stiffness matrices which are connected together by Eq. (1 ). The sub matrices of [ K] are shown in Figures 8 & 9 for the two versions. The [ B] and [K] numerical values are given in Appendix A Figures A-1 through A-4.

The subsystem stiffness matrices were computed by means of the EASE structural analysis program. The thermal plate and sunshield plates were divided into about 7 5 and 100 triangular finite elements respectively. Subsystem attachment nodes were given unit loads to develop the flexibility influence coefficient matrices.

The brackets were also modeled as plate elements making up the !langes, bases, and tops. Also, since the lateral forces due to the subsystems are being considered at the at the top of the brackets, but the base motion is at the


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bottom of the brackets, the rigid body forces will tend to deform the plate and give the bracket top more lateral flexibility than just the bracket flexibility as determined by the EASE program. This type of analysis gives the addi-tional "u" deflections associated with the three main subsystems in the [ B J matrix, and it gives the lateral stiffness matrices for these subsystems in the large [ K) matrices.

2. 2 Mass Matrix

The mass matrix in generalized coordinates was developed from the c. g. mass data of the components involved. This transform.ation is as follows:

[M) q

= [ c] T [ M] [ c] q

(3)

where the mass matrix [ MJ is the diagonal matrix of c. g. mass character-istics and the matrix [ G] is~he relationship of the c. g. coordinates {p} in terms of the generalized coordinates { q}

{p} = [C) {q} (4)

These matrices are given in the Appendix as Figures A-5 through A-8.

2. 3 Forcing Matrices and Input Levels

The forcing matrices are functions of the base acceleration and the transformed mass matrix as follows

(Forc~n~ = [C) T [ M) {p0

.1 tMatrlx) P

where the matrix {p 0 } is the column matrix of applicable base motion coordinates, i.e., X , Y etc. depending on the excitation direction.

0 0

The input levels (design limit) at the LM interface are shown in Figures 10 and 11 for sinusoidal and random vibration respectively,


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3. 0 COMPUTED ACCELERATION RESPONSES

The computed responses at various points throughout the structure were obtained for each version of the Array E and are presented in the form of curves of transmissibility, sine response and random vibration response as well a-s Tables of RMS values of accelerations at various locations.

Initially the normal mode shapes and natural frequencies were calculated resulting in 32 mode shapes and natural frequencies for the LSG version and 30 mode shapes and frequencies for the PSE version. The many numbers involved here are reduced to those of Table 5 where-in the frequencies are listed along with the largest responding coordinate.

These natural frequencies are in the general range of previous Subpackage-1 natural frequencies as would be expected. The lowest plate mode frequency of about 50 Hz appears in many previous test re-sults.

The other resonant frequencies are all associated with a particular motion as indicated in Table 5. The highest frequencies in this dynamic model are around 1300 to 1400Hz; thus no computed response occu·rs much past these frequencies.

Computed freq\+ency responses for sine and random inputs were obtained for most of the generalized coordinates, and in an effort to re-duce the quantity of data presented many of the response curves are pre-sented in one figure. Table_~_of ov:erall G-H.MS responses are also pre-sented for easier comparison. These values have been selected from the response curve value or were obtained by averaging two or three sets of values for one package. Tables of G-RMS values are presented in Table 6 for the LSG version and Table 7 for the PSE version.

: : .-· ..

A damping factor of 10% of critical viscous damping was used in all modes except the ones involving the LSG resonances where 15% was


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used. This will tend to be on the conservative side since previous Sub-pack- I tests have indicated somewhat higher damping. Another factor not in the analysis is the pin clearances at the LM interface. This reduces the actual transmissibility from the shaker to experiment subsystems in the measured results,. particularly in the lateral directions Y & Z and at high frequencies, giving slightly more conservatism.

Response curves that are included in this report are presented in the coordinate number order so they can be located using Table 3 and/or Figures 1 & 2. A typical set of curves for a given coordinate response might consist of the in-axis transmissibility and sine response, and the combined random responses due to the in-axis and the cross axis excita-tions. Also shown on the sine and random response figures are the design specification values from Reference 2. For the random vibration spectrums, the in-axis response curve is presented as a solid line. The numerical value on the upper corner of the grid is the in-axis G-RMS value.

Details of the computer program used in the analysis are given in Reference 3.

Most of the curves presented were calculated for the LSG version, and, unless the computed responses for that location in the PSE version were appreciably different, the PSE version curves are not presented in this report. Unless noted, then, the curves of response for the LMS, LSP and other locations can be considered to apply to Array E, SP-1 versions.

3. 1 Computed Responses at Specific Locations

The response curves are presented in successive numerical order for the generalized coordinate numb1:lr designated as "location 11 on the curve. For the LSG version these are Figures 12 through 30 and for the PSE version Figures 31 through 33. The LMS was hard-mounted to its brackets in all the calculations except the ones so designated in the LMS response curves. These are the cases where the rubber grommets were included in the analysis. There was little difference in effect on other subsystem responses.

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LMS responses are given in Figures 12, 27, and 28 & 29 for the X, Y, and Z axis responses. Some peak values for the random launch and boost responses exceed the specified value curves in amplitude but the overall rms response value is still fairly low. The effect of the rubber grommets is to lower the natural frequencies and the peaks somewhat with the largest effects occurring in the Z axis. Here the largest in-axis peak response (Figure 28c) is decreased appreciably (Figure 28c~

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sun-shield and thermal plate. These responses also form part of the response for the electronics packages below. There is considerable higher frequency response at 500 Hz and up, and the cross axis responses are sizeable.

Figure 18 shows the random response spectrum for the LSP electronics package on the thermal plate. This and the four part Figure 19 (for one of the transmitters) are typical of the thermal plate package responses.

The LSG responses are presented in the six Figures 20-25. In this case isolators in all three axes are used between the bottom of the package and the sun shield. Thus the lowest mode frequencies in the system occur for this 111ubsystem, i.e., 31. 0 and 43. 4 Hz. The largest dynamic deflections will likely occur for this package also. The motion responses were calculated for both the LSG, c. g. Figures (20-22) and the bottom corner responses Figures (23-25) just above the isolator attachment. In general the high frequency responses are attenuated as planned and the sine responses in the Y and Z directions for the c. g. (Figures 21b and 23b) respond at the lowest frequencies. The overall rms responses to ramdom inputs are all quite low even though an occasional peak value (Figure 25c) exceeds the specified curve level.

The LSG isolators were selected on the basis of the work dis-cussed in Reference 4 wherein the responses of the c. g. when excited by the specified levels of Reference 2 are presented. The corresponding curves in the present report are those of Figures 20-22 as mentioned pre-viously, and comparisons reveal that the presently computed levels are all appreciaMy lower than those of Reference 4 which were considered to be a satisfactory environment for the LSG.

The final set of response curves presented is for the PSE version of Subpack-1. These are Figures 31, 32, and 33 for the X, Y, and Z PSE package responses as calculated at the bracket/experiment interface. The overall responses indicate that the input levels fron'l Figure 11 are attenuated, but there the usual peak values of power spectral density occurring at the system resonances. As stated earlier, only the PSE response curves are presented here for the PSE version of Array E

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.,

since the other computed locations did not differ largely from the same location in the LSG version.

The computed PSE response curves have been compared with some of the Subpack 1 Qual test data and found to be of the same order of magnitude in RMS value and to have a similar shape at the low fre-quency end. The previous test result curves are presented in Reference 6. Of the three sets of test data, Qual C data is the closest to the pre-sently calculated responses. Overall the PSE should not see a more severe environment in Array E than it has been subjected to in previous arrays.

In general there are no unusual or severe vibration response pro-blems indicated by this analysis. The results are in general agreement with previous Subpack 1 test results although in two instances, the LSP Y and Z responses (Figures 26 and 30), the fairly large deviations of the PSD peaks from the specified curve indicate that these points should be monitored during the Engineering Model testing in order to determine if this level of high frequency response a.ctual.l.y exist•.

4. 0 DYNAMIC LOADS

The internal loading in the structural assemblies were calculated by a process of inserting the product of mass and acceleration into the original stiffness matrix and computing the internal loads and deflections for the coordinates of Tables 4a and 4b. Details of the method of calcu-lation are given in Reference 3. The objective here is to be able to com-pare the loads with the "quasi- steady- state" design load factor assumption of 20 g throughout the structure.

Calculations were made for both versions of the Array E SP-1 but only the LSG version loads and deflections are included here. The PSE version loads do not differ appreciably in those cases where direct comparisons can be made.

A listing of the worst case loads due to x-axis sine excitation is shown in Table 8. This occurs at 54.5 Hz. The highest loads here are indicated to occur at the LSP attachment points, u 1 0, u 11., u t2, u 1 3, but this is due to the rigid body assumption for this package. The loads shown

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here would be relieved somewhat by the package tab bending and the racking deflection of the package.

A listing of the worst case Launch and Boost random loads and deflections is shown in Table 9 for the LSG version. These are root mean square values (one sigma) and should be multiplied by 3 to compare with a 30 g load (20 g load factor x 1. 5 factor of safety) at a particular location.

Lunar descent environment loads are all less than those shown in Table 9. The coordinate location numbers correspond to Table 4a.

An interpretation of the load figures of Table 9 is given in Table 10 where direct comparisons are made between the various subsystem dynamic loads and the design load assumed initially.

For the first 3 _subsystems, the LMS, LSP and LSG, the. loads are those occurring at the top of the bracket at the experiment/tab inter-face. The third column of figures is the root-mean-square (one sigma) load value obtained at the coordinate location indicated in the first column. The numbers are multiplied by 3 to obtain a 3-sigma load for comparison with a 30 ~ ultimate design load factor at that location. For the LSP and LSG, two brackets carry the computed load in the lateral directions at each end of the package.

In the remaining cases, i.e., thE;~ntenna cable reel, electronics packages, etc., the Table 9 load represents the load at the c. g. of the designated package. These loads are in the X-axis direction only. Calcu-lated loads in the Y and Z lateral directions for these components would be about half the magnitude of the 30 g design load column figures.

An assumed design load factor of 30 g on ultimate in the present case was a safe assumption throughout the structure as can be seen by comparing the last two columns in Table 10. The last column figures are 25o/o or more greater than the 3-sigma loads.

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5. 0 REFERENCES

1. ATM 268 ALSEP System Mass Properties, 6 Nov 70.

2. Letter No. 9712-56, Array E Subpack #1 Subsystem Dynamic Environment, 15 Oct 70.

3. BSR 3095 "Dynload" An Integrated Dynamics and Loads Analysis Pr~gram, March, 1971.

4. Letter No. 984-ME-007, Isolation of the LSG from its Vibration Environment.

5. ATM 832, ALSEP Qualification Design Limit Vibration Test Data Summary, 27 June 69.

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Array E Subpack I Dynamic Analysis PAGE 12 OF-

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A LSEP ARRAY E WEIGHT ESTIMATE

SUBPACKAGE #1 Configuration

Prime Alternate

C/S and LSP/CSE 44.2 N/A C/S and LSP & PSE CSE N/A 48.4 Primary Structure 9.0 9.0 Sunshield Assy/Sub/Fast 12.0 12. 0 T/C Curtains 2.0 2.0 Boom • 9 • 9 PDM 1.0 1.0 Sunshield Extenders 1.0 1.0 Antenna & Cable 1.3 1.3 Antenna Mast • 8 • 8 Fasteners 1.0 1.0 LSG/Cable 26.2 N/A LSP/Geo/Ant/Cable 11. 2 11. 2 LMS/Caple 22.7 22.7 PSE N/A 22.3 Miscellaneous 1.0 1.0

Total 134.3 lb. 134.6 lb.

TABLE 1


ALSEP ARRAY E CENTRAL STATION ASSEMBLY

DETAILED WEIGHT BREAKDOWN (ESTIMATE)

Data Processor /Multiplexer CMD Receiver Diplexer Filter Filter Switch Transmitters (2) CMD Decoder PCU/PDU Thermal Plate & Hdwe Harness Assy Thermal Bag PSE Elect. LSP Elect. Miscellaneous (includes Ant. Cable)

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4.20 2. 50 1. 00 1. 30 4.20 3.20 8.00 9.00 2.50 l. 50 4.20 4.30 2.0

48.40 LB.

(44. 20 LB. less PSE elect.}

NOTE: All weights are estimates based on previous ALSEP Models.

TABLE 2

1

2

3

4

5

6

7

8

10

11

12

13

14

15

16

17

18

19

20

21


TABLE 3

GENERALIZED COORDINATES (REFER TO FIGURES 1 & 2)

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LSG Vets:lon PSE Version

ul. } u3

u3

Ul3

Ul4

u15

Ul6

Ul7

u18

u19

U20

u21

LMS

Boyd Bolt Near LMS

Cable Reel

Antenna

Below

LSG

on Sun Sh.

LSP

Boyd Bolt RCVR, DIPL

Boyd Bolt RCVR, DIPL

PCU/PDU i

iCOM/DEC I l

Thermal !DATA/PRO.

Plate lDIPL/SW

C omponent~LSP /E LEC ~

fMTR

lxMTR

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

16

17

18

19

20

21

1 LMS J

::} u4

u1z

u13

U14

u15

u16

Boyd Bolt Near LMS

Cable Reel

Antenna

PSE

LSP-Geophones

Boyd Bolt !RCVR, DIPL I

Boyd Bolt !RCVR, DIPL

Thermal

Plate

PCU/PDU

iCOM/DEC

!DATA/PRO.

'orPL/SW i

u 18 ComponentsiLSP/ELEC.

Ul9 j !XMTR u 20 ixMTR

u21 IPSE/E LEC.


NO. I REV. NO. ATM 989 ,,

PAGE 15 OF ~ £vstems Division

DATE 5/24/71

TABLE 3 (CONT)

LSG Version PSE _Version

22 ul LSG u LSG 22 VI

} 23 u2 at v at 23 v2 PSE 24 u3 Isolators w C. G. 24 WI 25 VI e 25 VI

} 26 WI ljJ 26 v2 LSP-Geophones 27 VI J LSP 27 WI 28 WI 28

vz \ 29 v2

} 29 ~2 LMS

30 w2 LMS 30 wi, w3

31 w3

32 v2 LSP

1 ul } 2 u2 3 u3

4 u4

5 us

6 UI

7 u2

8 U3

9 u4

lO u1

11 u2

12 U3

13 u4

14 u14

15 u 15

16 ul6

17 '17

18 ul8

19 ul9

20 u2o

21 u21

22 u22

23 u23

24 U24

5 u


TABLE 4a

SUBSYSTEM COORDINATES ARRAY E SP-1 (LSG VERSION)

LMS 26 U!

~'< ';~ :; .. 27 u2

Boyd Bolt Near LMS 28 u3

Cable 29 u4

Antenna 30 VI

31 v2 Below

32 LSG

WI LSG

33 w3 on Sun Shield

34 u{

35 ul Isolators: uf 36 Sunshield 3

LSP 37 l Connection end u4

38 vl } LSP Boyd Bolt 39 w1 Boyd Bolt 40

VI l 41

:: J 42 LMS 43 w2 . 44 w3

Thermal 45 V2 } LSP Plate 46 w4

NO. RI!V. MO.

ATM 989

16 PAGI! OF

DATE 5/24/71

1 ul

] 2 u2 3 u3

4 u4

5 us

6 u1

7 U2

8 u3

9 u4

0 u1

11 u2

12 u3

13 u4

14 ul4 15 ul5

16 ul6 17 u 17

18 u18

19 ul9 20 u2o 21 u21 22 u22

23 UZ3 24 I

llz41

:2J

26

. -Array E Subpack I Dynamic Analysis

TABLE 4b

SUBSYSTEM COORDINATES ARRAY E SP-1 (PSE VERSION)

LMS 27 vl PSE 28 V2 Above

Boyd Bolt Near LMS 29 wl

Cable 30 w3 Antenna 31 vl

32 v2 t~~~·

PSE 33 WI Above

34 W4

35 V!

36 v2 LMS

LSP 37 v3 Above 38 W2

39 w3

Boyd Bolt

Boyd Bolt

Thermal

Plate

NO. Rf!V. NO •

ATM 989

17 PAGE OF

DATE 5/24/71

NO. REV. MO.


PAGE ·18 OP

Aeroapaoe ····-~Division DATE 5/24/71

1. 2. 3. 4. 5. 6. 7. 8. 9.

10. 11. 1. 2. i 3. 14. 15. 16. 17. 18. 19. 20. 21. 22. 23. 24. 25. 26. 27. 28. 29. 30. 31. 3 2.

TABLE 5

NATURAL FREQUENCIES AND RESPONDING MOTIONS

LSG Ver,sion·

Freq.

(H~) 31. 43.4 54.8 75.4 82.0 95.0

103 118 125 132 145 147 152 162 183 212 230 256 259 323 385 399 434 460 496 529 640 769 953

1153 1277 1411

Motion ..

LSa· Rot* about z axis LSG Rot, about Y axis Lowest Plate mode X LMS Z Th. Plate 16, LSG X LSGX Th. Plate 16 Th. Plate 19 LSP X Th. Plate XMTRS LSGY LSGZ Th. Plate 17 Th .. Plate 17, LMS Y LMS X, LMS Z LSPX Th. Plate 18 Th.Plate 18 LMS Rot. about X Ant. Cable Th. Plate XMTRS Th. Plate XMTRS LSPX LSP Y Center Boyd Bolt Antenna LSP Rot.abou't'-x axis

Under LSG X

;~ Rot. = Rotation

1. 2. 3. 4. 5. 6. 7. 8. 9.

1 o. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. 23. 24. 25. 26. 27. 28. 29. 30.

PS~ Version

fteq. (ftz) 53.3 69.8 81.6 88.6

103 113 123 126 129 138 145 161 171 201. 223 241 254 283 302 347 373 398 421 448 475 535 576 610 640

1280

Motion. Lowest Plate Mode X Th. Plate 21 Th. Plate 14 Th. Plate 21 Th. Plate 15 Th. Plate 19 PSE Z (24) LSPX PSE Y Th. Plate 20 Th. Plate 16, LSP X Th. Plate 16, LMS Y LMS X, LMS Z Th. Plat~ 17, 20 Th. Pia te 1 7, 1 0 Th. Plate 17, 9 Th. Plate 17, 4 PSE X Ant. Cable X FSE X Ant Cable & 13 Th. Plate XMTR Boyd Bolt 12 LSP Y LSPX PSE Y Ant Boyd Bolt 13 LSP Rot. about X Boyd Bolt 12

Input Axis


TABLE 7

ARRAY E SP-1 VIBRATION ANALYSIS RESULTS (PSE VERSION)

Root Mean Square Response (G-RMS)

X y

' ~·· Response

Subsystem Axis L&B L.D. L&B L.D. L& B

PSE X 4.0 I. 85 1. 72 1. 25 1. 87 @ y 3.6 I. 60 2.7 2.00 0.88

Bracket z 2.7 1.18 0.56 0.40 2.39

X 3.7 I. 71 2.0 1. 39 1. 66 LMS y 0.96 0.44 2.78 2.05 0.8

z 2.5 1. 21 2.16 1. 53 3.66

LSP X 3.3 1. 70 2. 36 I. 67 2.82 y 1.1 0.47 4.86 3.44 5.85

Geoph. z 0.73 0.35 2.54 1. 72 7.78

Recvr. X 3.17 I. 79 3.01 2.12 4.54

C/D X 2.3 I. 73 0.42 0.33 0.99

Xmtr.· X 2.94 I. 58 1.25 0.90 0.91

DA/PR & X 3.22 1. 55 1. 86 I. 32 1.77

LSP/CSE

PSE X 2.2

Elect. I. 59 0.17 0.13 0.9

z

NO. {1 RI!V. MO. ~:"

ATM 989

PAGE 20 OF

DATE 5/24/71

L.D.

1. 07 0.46 1. 73

0.92 0.49 2.11

1.40 2. 68 3.83

2.19

0.81

o. 62

1.14

0.77

NO. ~ Rf!V. NO.

Array E Subpack I Dynamic Analysis ATM 989 I I PAGI! 21 OF

=-~ DATE 5/24/71 ~,~~. TABLE 8

SINE LOADS AND DEFLECTIONS @54. 5Hz

Coord. Coord.

No. De fl. Loads -lb. No. De fl. Loads-lb.

1 . 0104 5. 9 25 • 02186 12.7

2 . 00762 19.7 26 • 016397 -61. 4

3 . 02565 182.9 27 .. 024985 110.9

4 . 01022 7. 5 28 . 02572 I52. 5

5 0 00462 2.6 29 • 017I35 67.4

6 . 02564 -52. 1 30 . OOI2I3 10.8

7 . 0083 I 12. 2 31 • 001213 10.8

8 . 00279 I 53. 5 32 . 002764 24.5

9 . 006997 68. 5 33 . 002764 24.5

IO . OI 598 I78. 34 . 02564 61.4

II . 002115 -172. 35 . 008307 -ll o. 9 I2 . 0086I I97.2 36 . 002794 -152.5

13 . 02305 -147.3 37 . 006997 -67. 4

14 . 02372 75. 9 38 0 000784 36.

I5 . 02186 38.3 39 -. OOOI13 o. 5 I6 . 027575 38. 3 40 -. 00396 -41. 5

17 • 02949 27. 2 41 -.003578 -I4. 5

18 . 0369 37.4 42 -. 003197 -44. 5

19 0 02449 5.4 43 -. 00697 5 I6. 1

20 . OI54I I5. 4 44 -. 00881. -115. 7

21 . 014259 5. 4 45 . 000782 35. 8

22 . 01053 4.3 46 -. 000112 o. 6 23 . 03587 -4. 2

24 . 02372 -57.6

( LSG Version)

"l

DEfUCHONS 11\ifERNAl. UlADS

.,. )(' 1 o.zc.ztt>l~>E-'J1 n.a5ll!C.Il2E 02 2 'O·lSOll!U-'::2 0.3922,ti27ff 02

. 3 o • .5;.c ~;-;1 '5~-cz ____ c.-t:z·;.H-!IBE 02 __ 4 .o.l9l75H-E-C3 n.I·o:rst> 7ZE cz t C.H3ZHZ-f-'(2 __ 0 • .Sl>O 1-€ 7.5E CZ __ 1 9ol6(;.t,Q.t.993263f 02 f! (. H7o02 e c ... nsnat-~3 ~------0.3'8M067E 02 = 1il t:.-f:!Ulll£-03 _ -o.34153HlE 1>.2

lfl c. 3372461£--cz ~.546711~ 02 H e.~"9'H84f'-G3 -- -··- - .0.2047395€ 02 ---12 O.Hl9Cl6E-OZ --· 0.3113501£: oz --13 ().3412'>27£-0Z O.ZOlo1:16)E 02 -14 o. 323.Sit03£-CZ __ .1:l.12HOSOE 02 1~ O.Ztil2BSE-02 o.an3303E 01 It 0.2514892£-02 t). 25 2 7495£ 01 11 o. H:05C4'5E-CZ ____ Q,lZ4.5683E 01

_ 18 .C.21:44937H23E-03 ----- _0.34606'51£ oz 3f C.8389773E-C3 o. 3178055[ 02 3'i C.910412lE-03 _______ 0.48604l6E 02 40 0.144i813lE-OZ ____ .. ___ 0,2782041E 02 ~1 C.l~7H89E-OZ ______ 0.9269849£ 01 42 0.153123 7E-CZ o. 2811 931E 02 4~ 0.213t5S5E-02 .. ______ O.l31214lE 02 44 O.l4C7C5BE-CZ _O.l185106E 02 .t,5 c.e77C570E-C3 0.3472220[ cz 4~ c.~4-.~2~2E-o3 - . ..0 • .5325711£. 02

)

___ OEflE\:JlOIIIS __ _.It-!T£RMt.. t.OAOS --- ~- ----~---- --r-- -------... l C.l!il5.34266l''i£ 01 t c. !"t24!"83£-0l __ 0.4f>24474E 02 7 c. 24i9'i511E-02 ___ 0.6902133E 02 _

__ s. o. 54346841'-03 - l).lo93 .. 15 .. 'E ~ --'i 0. 9Mll4U:-03 O.fl346570£ 02 ____

Hl c. 3364l8"'if-02 ().467l3'0U: ~ 11 c.t043436£-C3 - -- o. 4461186f>E 02. 14: C.17"i"iBCE-CZ o.soe6446t: 02 l~ o. 4t2~29'tt-C2 0.397(179t)E 02 14 c.512E782E-02 ____ 1l.2l

5/24/71

TABL:F; 10

Comparison of Launch and Boost Dynamic Loads

with Static Design Loads

Table 4a Sub- and Table 9 Three

System Table 9 Local L&B Sigma 30g* Coord. Coordinate Load-U Load-U Design Load-U

LMS 1 U1 85.2 255.6 515 z uz 39.2 117.6 420 3 U3 62.6 187.8 515

40 vl 27.8 83.4 165 41 Vz 9. 3 27.9

j 42 V3 28.1 84.3 43 wz 24.8 74.4 44 w3 23.8 71.4

LSP 10 U1 47.8 143.4 332 11 uz 72.5 217.5 l 12 U3 63.5 190.5 13 U4 42.6 127.5 38 V1 31.7 95.1 zoo (Two brackets) 45 Vz 34.7 104. 1

J 39 Wt 48.6 145.8 46 W4 53. 3 159.9 LSG 26 U1 55.6 166.8 416 (Two brackets)

27 uz 69.8 189.4 28 u3 75.3 225.9 29 U4 80.3 240.9 30 Vt 55. 1 165. 3 31 vz 55.1 165. 3 32 Wt 38. z 114.6 34 W3 38. z 114.6

Ant. Cable Reed 4 U4 18.6 55.8 102

Antenna 5 Us 10.8 32.4 47.4

PCU/PDU 16 U16 11.5 34.5 179 CDM/DEC 17 U17 9. 0 27.0 108 DATA/ PRO. 18 U18 11.4 34.2 126

DIPL/SW. 19 U19 3. 0 9. 0 28.8 LSP/ ELECT. 20 Uzo 10. 3 30.9 117 XMTR 21 u21 4.6 13. 8 45.6 XMTR 22 .~az:.,·· .. 4.6 13.8 45.6 Load at th.r3 12. 1 36.3

... ,,. 116 . 23 •

plate end · 24 uz~ 13. 3 39.9 116 ...,£Boyd 25 Uz.5 10.4 31.2 116

blts y

/?'/?

' * Includes a 1. 5 factor of safety

ARRAY E SU CKAGE NO. 1

-FIXED ANT. ---w ~·· O/"\f1~ _______---r( rlSP ANT. MAST

lSG

Figure l. Corpplete Ass,embly, LSG Ve/sion

8310N-IO-A JaiJ (Jl'"'d "--!U Nc;q *"'Cb "::J-N -~

NO. REV. NO.

~™ 989 Array E Subpack I Dynamic Analysis

25 PAGE OF

DATE 5/24/71

-g ) 1.A.r A (v.-L'{

1 v-

X>u ·---------·--

22 (U.) 2 5 (V")

9\'~--'--+' ----~,:-;)-"'ffi 6 i?6(UJ)

, ·~--24

,.,

0 Mass Lumped

7

1c --------llo

I MO. ~TM 989


PAGE 26

I RI!V. MO. •

OF

DATE 5/24/71

1

L X(uP)- Y

0 TX ~ZI )

-~AT: :;oc I 17

.DI PL.- FILTe'R.

E ~ -·- ...

I ,, ___ ___.I 31

I RECEIVE1?.

,_-----'---.

COMM. ffi \3 JYE:CODcR..

0 16

PCLJ /PDU 0 15

rr-~x ozo l L ____________ __;

'------~

LSP/C~E I EB o 1 4, ICl I I !

I

~ I

....._ ______ 1 1··-·--·-···-···-·------l 1 I

u : i I I ) L ··t.../ __ __;

I I

I ! l

I l I I

L-----------~-------·-··

I -... J

0 Mass Lumped

E£1 Connected Points (b~tvie·e.n> sun shield ~ th~rmal ~late)'

Figure 1'\)

Array E/Sub Pack 1, Thermal Plate (LSG Version)

(View From Top of Cut Away Sun Shield Plate)

L X(UP) y

0

NO. I RI!!V. NO.

~ ATM 989 Array E Subpack I Dynamic Analysis PAGE 27 OF

DATI! 5/24/71

-------- - .. ---~ --·-·~--.~·---··~~-·- -·-- .. (

LMS

PSE LSP

Mass Point

q (U}

I ; 1

I

25(\T) \

Z?(W)!

Connected Points (b'_etJe,en sun shield &i th~; nfai: plat1:1) 1

\

Figure 2a

Array E/Sub Pack 1, Sunshield Equipment (PSE Version)

(View From Top)

I ~---


~l ~.w. o 1

17 I

0 Mass Lumped

NO. REV. NO.

ATM 989

PAGE 28 OF

DATE 5/24/71

'

E9 Connected Points (1>et;J,e,en sunshield & t~ermal plate) ''

Figure 2b

Array E/Sub Pack 1, Therrnal Plate (PSE Version)

(View From Top of Cut Away Sunshield Plate)

5/24/71

PREPARED lt\' (3. M Jt\)

CHECKED 8-Y----

ItEVI$ED SY

EN .. OIREEIING I!POIT DAT!~"'/=:t;) /71 PAGE 29

L. s .. c;. II

~ . ··-- ----....... LQ! D -------4111-J...-oj i -,

f -- --- --~]-~-...... ____________ _

---1

I ·.r ~

1 \!},

l • v w •. -···

~ Systems DMslon REPORT N•··-----

I I 0 00, I ~ ... , .. ,. ~-.-----· --····-~--··•"'': -~-~---~--- ------ ----------~

I

lil:

~:

I _t !

·~-, c·' -~ "-"'

-:>, I. . I &l!....RTO~.S • ~·..::> • l " I o.o i

/ '-'!' .. v·c-1 ;:: ---.. -··----·----- ------

Pu7)H:

~-- -------------------·- ----·----~-----------·------- --~

0

! I

I

' (\'' a) I 0. ol o-' -·I I I

lh . ---

mx = m = m~ = . 06:78 y f

about·c. g;·

' · ..... '2 lb-sec

in

l =1 . .3049 fn-1b2.s'~c2 X

i !

I I = Iiz. = 1. 6 8 2 in -lb - sec 2 y . . . >

i 0 @ L-.- ...... ________ _j

Figu:re(3 :r::;SG RquipmEmt

BxA-542

~;t!k)

PREPARED BY ___ _

CHECKED BY----

' REVlSED BY

,,

E.N .. OIREIEIIUNO REPORT Aaroapace Systems Division

I

13."2-r' -------

L /J.) ..

=j ,. . ... :; , , _:::..... ____ ~ __ !tiT ... L\J :rtl x, : 0 'l 2 , ;;:· :. ' ..• 05.p8..J.b -sec

5/24/71

! OAt! ___ PAG~dQ

REPOI!tT M•·-----

MOO!L L M s

in ,_ 1 _LMS Equ;i.pmen~ about' c. g; . ,. Ix = .. i. oJ~i lb -i~--s~~2 ~, . I I~

BxAS.C2

. i ( ~~

:::; • 7(,33 .i:' :440

lb-in-sec2 - 2 lb -in-sec

r-

5/24/71

PREPARED 8T G. tvf1N EN..OIR!EIINO REPORT DAtl!~/.:l0(71 PAGE 31 REPORT No. ____ _

MOOIL A L)Ef ARS F.. /S'PI CHECKED 8Y

REVISED 8Y

~vision

L. S. P. f.-

-,II .. ------- _____ --J ~

c &.

w = 11. 2 ,' lb

mx::: my = !nz = .• 029 lb-sec:;Z _· ' i i:tl, ,< I

about c. g.·

Ix ::: • 3602 }b-in-:-sec2 ' ':.:: ( J f~

Iy = • 483, lb .... in-sec2

Iz = • 360·2 '.1b-in-sec2

•. .J'_'t' ·•"

!

-r·· ~ I I'· I

i I ! y

J cr-1

~I _L_

I

. ~~ ---------------

I) F5l t;j

I ,_. ___ ... ___ ?>.9-7.5_'1 _ --- ----

/• _... . ------- ____________ j ___ Q .. ---- ---- ------- ·--';9r

Ffgure SfJ..SP Equipmr_ent)

~------------------------------------------------------=-· mas~ L-----------~ 8xAS42

PREPARED av G . M 1 tJ CHECKED lilY ___ _

ltEVJSED ltY

p, :::. J::.

I

1--i 1

1-o&----- ..

. . about c~ g,

~X = ~ 1662,

Iy = Iz = 1., 306 1 in-1b-s~r2

1 •• t t t :. ~.... - , .. r·

EN .. OIMEEIINO REPORT Aerospace Systems Division

----- ---------1 ~

'·/

5/24/71

DAtE 2-b

Figure 7

Computer Programs and Assumptions

~ -t .. l.n '-.... N ~

~ ......

: a Pi

w w

0 "'II

> ~ ..., . $': -.i)

00 -.i)

~--"' 1'1'1 :c :z ?


[K1] ....::-- Sutv SHIE-LD !=e. 15JC\5

l Kz] ~ THGlo"E (Ui)t;J,) 2X2

( K5] --E-LMS Aeo~E 5K5 l

(k~] -E-LSPAeo~r (u:.,v)t~-'1j ZX2.

l~J~ l_B]T [k]{B]

~ (32

[K] 3'1"~-3t)


[K,J ~ 5uN SHIELD~t5~ 15

::::. ( 30 l( 3 0 ')

I I

Figure 9 Sybsystem Stiffness Matrix (PSE Version)

I MO.

ATM 989

I R!!!V. NO. I

PAGI! 35 01'

DATE 5/24/71

SINUSOIDAL VIBRATION

SPECIFICATION LEVELS

Combined L & ,B ·-and Lunar Desc.ent

Figure 10

Input Axis:

Sweep Rate: 3 -Oct. /min.

Frequency (Hz)

440-90

Page 36 5/24/71

. l 10 9

8

7

6

5

• 0110 9

H-'

8 ~_:__..._. >,7 ....

..... 6 (I)

~ 5 Q)

o.

I'

lj il

i L1 I

i' l

I '

~~~ rt,. '' f11f

Frequency (HJ)

Figure 11. Random Vibration Specification Levels

Page 37 5/24/71

+'

I, 1 ; : t+J+H, -+-i'-H-H-t1

l:tlli r:-

·.·'

+-+-~··- -~+1·,

fT --l-

+-

r:t :±

1 ii 1 ; i-r·H' +++++t-Hi u ,,, l ,, ---' c:+tt+ ttl

. , . --'T''>~m H-i

0

Page 38 5/24/71

MM RLSEP RRRRY E/SP-l,F~RCJNG IN X-RXJS JAN. 1971 **

FIGURE IZQ TRANSM1SSIB1l1TY

LeJCATieJN 2

L MS X

~~ ~ :j

! Nl

! j .... i ~ ~"'-+-i -------+-----------+------------•. _.... en . ~ QO j ·_1 !"-

;:; w . ._, V)~ (f) .::11~

~ (T)~ L I (f) N~

~ I rr-:-o 1-- ....-1~====--

c:n a:> i"'-CD

N~ - I 'o

5/24/71

** RLSEP RRRRY E/SP-l,F~RClNG IN X-AXIS JAN. 1971 **

0')

~co r-

1 (/J 1./")

w (f)(Y)

z D !l...C\.1

en

FIGURE I :z b

Wo / a:Of

SINE RESP~NSE

...--.""-+--------. ----------1--+----------+--0')

co r-(/J

lf)

:::t'!

(Y)~ i

-ru~ 'o

-·----------------------~

-~--~------~~~--~~--~~~~~--~--~~~~ 1 01 3 LL s s .ffl9 1- cf 2 3 ij s Slffl s 1 a'

FREQUENCY (HZJ

>--,_ .......

_J

a: a: ,_ u w CL (/)

1'"1

Page 40 5/24/71

x* RLSEP ARRAY E/SP-l,F~RCJNG JN X-AXIS JAN.1971 ~

f 1 GURE I 2 c RAND~M VJBRATJ~N SPECTRUM

L~CRTI~N 2

3. 41.66 G-RMS

---------+----- -1---- ---~ I .

------

\

\~

~0-1 ~2--~3~~~.~s~s~~~s~1-if~~2~~3-~~s~s~~~s~1 ~if~~~~~rrrl FREQUENCY (HZJ

5/24/71

RLSEP ARRAY E/SP-1, FCJRC I NG IN X-AXIS (LSG 8c LMSJ

N I: "'-o C\JO

FIGURE I 2 c ~ RANOCJM VI BRAT I CJN SPECTRUM L ~B

LCJCATieJN 31.!

2. 7728 G-AMS I

~ ~~--------------~--------------+-------------~ ~ D

>-r-1--1

en z W-D'o

_l a: a: r-(_)

w Q._ (f)

~~--------------~--------------~------------~

(I')

'o

;-1 I

! I

-~--~--~~~~~--~--~~~~M---~--~~~~

r f

5/24/71

RLSEP RRR E/SP-1 (LSGJ , FCIR IN X-RX 1 S (LUNAR DESCENT)

F T G U Rf. I .:Z d RRNDCIM VIBRATION SPECTRUM

LCICRTICIN 2

-0 LMS -~------------~-------------~------------~

1. 5641 G-RMS

I :''.l I T j ,_ I ~/bl X -~-------------~--------------+-------------~ X

C) ~

z

_j ~~----------~-4--------------+-------------~ rr cr

~ ~ J) ~ a: C\J i :._u I

SPEC.

~::::J ,~~------~~~-4--------------+-------------~ a

(l_

('1'1

'o -~--~--~~~~~--~~~~~+-~~~~~~~

1 01 2 3 4 5 6 7 8 9 1 rf 2 3 L! 5 6 7 8 9 1 ct 2 FREQUENCY (HtJ

N 0

(j)

00 r-

5/24/71

** RLSEP ARRAY E/SP-l,FORCING IN X-AXIS JAN.1971 *~

FIGURE J.3b SINE RESPeJNSE

LeJCATI~N 3)ul

'b e (} y D e () L T X - ~e.:H"O t-JOE:

REC. ElY C. k J /)!Pl..,/

CM D. /.)ECoiJf ~} 1 1

IY e 1\ R._ L. 1'4 :;. e (IU·; I

2 s ~ s Mtes 1 ri 2 3 ~ s s 1 as 1 r:! 2 3 4 s s 7 ss 1 o" FREQUENCY (HZ)

-

Page 45 5/24/71

** RLSEP ARRAY E/SP-l.F~RCJNG JN X-AXIS JAN.1971 **

FIGURE f~C RAND~M VIBRATJ~N SPECTRUM

L~CATJ~N 3 I?~CEJvEN ; j)1PL. J

C/11), {)EC4J)Eie)

-o ~yv g,JL-t x- Re~t=aotJ6~ JY~Ai~ '-H s 8RKT

N I "-o No

------~-2-.-3669~-RMS 1

X ....... ""-i---------+--------+ ·-----------1 x (_')

>-!-~

(f)

z

(")

'o

... 0

Page 46 5/24/71

RL5EP RRR E/SP-1 (LSGJ , FCJR IN X-RX I 5 (LLJNRR DESCENT J

FIGURE !3d RRNOCJM VIBRRTICJN SPECTRUM

LCJCRTICJN 3

X- RE.SPOl-J$€ ~~--------------~------------~------------~

,....... N I "'-o (\JQ

x ....... )(

D

'>-!--........ J)

z u.J-=:J'o -..J a: cr ..__

.:._)

:..W n J)

a: !\I LL.J 'o :3: ....... 0 CL

"' 'o

J I

~ I

., I I I , . >I y I I I

'i" 6872 G-AMS I

--

,.-. >-,....... "'-1

_J ~

a::l ~

en en -L en 'Z a:

Page 47 5/24/71

** RLSEF ARRAY E/SP-l,F~RCJNG IN X-AXIS JRN.1971 *~

FIGURE \4a TRANSMISSIBILITY

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Page 48 5/24/71

** RLSEP RRRAI E/SP-l.F~RCING IN X-AXIS JAN. 1971 **

FIGURE ·14b SINE RESP~NSE

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5/24/71

** ALSEP ARRAY E/SP-l.F~RCING IN X-AXIS JRN.1971 *~

FIGURE l4C RAND~M VIBRATI~N SPECTRUM

L~CATI~N 6

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Page 50 5/24/71

RLSEP RRR E/SP-1 (LSGl , F CJR IN X-RX IS (LUNRR DESCENT J

FIGURE 14-d RANDOM VIBRRTICJN SPECTRUM

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Page 51

5/24/71

XX RLSEP ARRAY E/SP-l.F~RCJNG IN X-AXIS JAN. 1971 X+

FIGURE \;Q TRANSMISSIBILITY

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Page 52 5/24/71

** ALSEP ARRAY E/SP-l,F~RCING IN X-AXIS JAN. 1971 **

FIGURE /5b SINE RESP~NSE

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5/24/71

MM RLSEP ARRAY E/SP-l.F~RCJNG IN X-AXIS JRN. 1971 Mi

FIGURE 15C RRND~M V1BRRT1~N SPECTRUM

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Page 54 5/24/71

RLSEP RRR EISP-1 (LSGl, FCJR IN X-AXIS (LLJNRR DESCENTJ

FIGURE 15d RRNOCJM VIBRATICJN SPECTRUM

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Page 55 5/24/71

ALSEP ARRAY E/SP-1. FORCING IN X-AXIS (LSG co CGl

FIGURE \b RAND~M VIBRRTI~N SPECTRUM

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Page 56 5/24/71

RLSEP RRRR'f E/SP-1, FCJRC I NG IN X-AX I 5 (LSG ~ CGJ

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RLSEP RRRRY E/SP-l.FBRCING IN X-AXIS lLSG © CG)

FIGURE !8 RRND~M VIBRATION SPECTRUM

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MM ALSEP ARRAY E/SP-l,F~RCJNG IN X-AXIS JAN.1971 MM

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Page 60 5/24/71

MM RLSEP ARRAY E/SP-l.F~RCJNG IN X-AXIS JRN.1971 **

RAND~M VIBRRTI~N SPECTRUM

LeJCRTieJN 20

XM/1

5/24/71

""- RLSEP RRR E/SP -1 (L5Gl , FCJR IN X-RX IS lLUNRR DESCENT J

FIGURE lqd RRNDCJM VIBRRTICJN SPECfRUM

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RLSEP ARRAY E/SP-l,FDRCING IN X-AXIS lLSG © CGl

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5/24/71

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FIGURE =zo b SINE RESP~NSE

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Page 64 5/24/71

RLSEP ARRAY E/SP-1, FCJRCING IN X-AXIS (LSG © CGJ

FIGURE zoe RANDCJM VIBRATICJN SPECTRUM ~ ~: ,;;..-

PC~ge 65 5/24/71

RLSE.P ARRAY E/SP -1, F CJRC I NG IN Y -AX I 5 (LSG @ CGJ

FIGURE 2\Q TRANSMISSIBILITY

LLJCATILJN 23

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5/24/71

RLSEP RRRRY E/SP-1. FeJRCING IN I-AXIS tLSG co CGJ

FIGURE 2\b SINE RESPeJNSE

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Page 67 5/24/71

RLSEP RRRRY E/SP-l,F~RC1NG IN f-RXIS (LSG © CGJ

FIGURE Zl c RRNOQM VlBRRTI~N SPECTRUM

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ALSEP ARRAY E/SP-1, F~RC I NG IN Z-RX IS CLSG © CG)

FIGURE :zza.. "TRANSMISSIBILITY

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Page 69 5/24/71

RLSEP ARRAY E/SP-1, F~RC 1 NG IN Z-RX IS (LSG © CG)

FIGURE 2Zb SINE RESPONSE

LOCATI~N 24

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Page 70 5/24/71

RLSEP ARRAY E/SP-1, F~RC I NG IN Z-RX IS lLSG l9 CGJ

' FIGURE 2.2 c RANDOM VI 'BRAT I eJN SPECTRUM

5/24/71

** RLSEP ARRAY E/SP-l,F~RCING IN X-RXJS JAN. 1971 **

FIGURE c.3Q. TRANSMISSIBILITY

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Page 72 5/24/71

~* RLSEP ARRAY E/SP-1,F~ACJNG JN X-AXIS JRN. 1971 *

FIGURE 23b SINE AESP~NSE

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Page 73 5/24/71

** ALSEF ARRAY E)SF-l.F~RCING IN X-AXIS JAN.1971 **

F 1 G U R E c 3 C R R.N 0 ~ M V I 8 RAT I ~ N SF E C T RUM L ~ p;,

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Page 74 5/24/71

ALSEP RRR ElSP-1 lLSG) , FCJR IN X-RX I 5 (LUNAR DESCENT)

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Page 75 5/24/71

** RLSEP ARRAY E/SP-l,F~RCING IN Y-RXJS JRN. 1971 *~

F I GUAE 2.4C\ TRANSMISSIBILITY

i_~CATTeJN 25

3 4 5 6 7 88 1 Q2 2 3 4 5 6 7891 IT' FREQUENCY (HZ)

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5/24/71

** RLSEP RRRRY E/SP-l.F~RCJNG IN 1-RXJS JRN.1971 **

FIGURE 24b SINE RESF~NSE

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5/24/71

ww RLSEP RRRRY E/SP-l.F~RCING IN Y-RXIS JAN.1971 ~

FIGURE 2.4-C RRND~M VIBRATION SPECTRUM

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Page 78 5/24/71

ALSEP ARR ~/SP-1 (LSGJ , FCJR IN Y -AXIS (LUNAR OESCEN TJ

FIGURE 24-d RANDOM VIBRATION SPECTRUM

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Page 79 5/24/71

** ALSEP ARRAY E/SP-l,F~RCING IN Z-AXIS JRN.1971 ~

FIGURE 25 a... TRANSMISSIBILITY

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Page 80 5/24/71

** RLSEP ARRAY E/SP-1.FORCING IN Z-RXIS JAN.1971 *:

FIGURE zs b SINE RESPCJNSE

LCJCATION 26 --tv"/

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Page 81 5/24/71

ww RLSEP ARRAY .E/SP-l,F~RCJNG IN Z-RXIS JRN.1971 MM

FIGURE 25c RAND~M VI BRAT I ~N SPECTRUM L. $ 8

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Page 82 5/24/71

ALSEP RI1R E/SP-1 (LSG) , F ~R IN Z-AX IS (LUNRR DESCENT J

FIGURE 2Sd RAND~M VIBRRTI~N SPECTRUM

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I Page 83 5/24/71

~~ RLSEP ARRAY E/SP-l,F~ACING IN l-RXI5 JAN.1971 **

FIGURE 26a. TRANSMISSIBILITY

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Page 86 5/24/71

RLSEP RRF1 E/SP-1 CLSGJ • FCIR IN Z-RX IS (LUNAR D,.ESCENT J

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Page 89 5/24/71

MM RLSEP RRRRY E/SP-l,F~RCING IN Y-RXJS JRN.l971 MM

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Page 90 5/24/71

ALSEP ARRAY E/SP-1, FEIRCING IN Y-AXIS (LSG &c LMSJ

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Page 91 5/24/71

RLSEP RRR E/SP-1 (LSGJ • FOR IN ( -RX I 5 (LUNRR DESCENT J

F T GURE 27d RRNO~M VIBRATION SPECTRUM

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)-

t-,__. 1..11 z w ... D'o -_J a: (L

t-u w ()._ (f)

PI

b -~---~--~~~~M-~~--+-~~~M---~--~~~~

2 3 ij 56 789102 2 3 L! 56 7891 03 2 FREQUENCY (HZl

>--0

Page 92 5/24/71

~~ RLSEP ARRAY E/SP-l,F~RCING IN t-AXIS JAN. 1971 ~~

FIGURE 2Ba. TRANSMISSIBILITY

L~CRTICJN 30

'2 -· R. E: '5 'POt·\:::.. E- ·---- -l ! i

~ ......... ~--- ---l·-----------·······--···----··-·· -----. ·----- -~ ,.._... 0)

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roll) ,.._... (D::t'

en ,.._..('I')

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-

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FREQUENCY CH:Z)

.~-

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lf)

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Page 93 5/24/71

** RLSEP ARRAY E/SP-l,FORCING IN lLRXIS JAN. 1971 MM

FIGURE 28 b SINE RESPCJNSE

LCJCRTICJN 30

. I

ru~ I I

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w ::1' en ('t") z E)

0... C'\.1

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lf)

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('t")

ru

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1 01 2 02 2 3 4 s 6 7 as 1 cr 2 3 4 s 6 7 as 1 oli FREQUENc·r (Ht)

5/24/71

ALSEP ARRAY E/SP-1, FCJRC I NG IN Z-AX IS (LSG ~ LMSJ

FIGURE ~8 h~ SINE RESPCJNSE

LCJCATICJN 30 N 0

([) -0

~~--------------~--------------~------------~ 0') t.=:)(X) ,.._ ,c.o

Ln

... 'o

·I I

~~~~--~~~~~--~--~~~--~--~--~~~~ rj 2 3 4 56 9 rf FREQUENCY (HZJ

>-}---

Page 95 5/24/71

** RLSEP ARRAY E/SP-l.F~RCING IN l-RXIS JAN. 1971 *~

FIGURE 28C RAND~M VIBRATI~N SPECTRUM

L~CRTI~N

LMS

2. 8524 G-RMS

I

I I I ~----------- ·---------~ I I I I

I

5/24/71

RLSEP ARRAY E/SP-1, FOAC I NG IN Z-AX IS (LSG &c LMSJ

N :r: ""-o (\JQ

FIGURE ~~ c~ RANDOM VIBRATION SPECTRUM

LOCATION 30

1 . 7904 G-RMS

~ ~~--------------+---------------~------------~ X c..:>

>-1--

5/24/71

RLSEP RRR E/SP-1 (LSG) , FOR IN l-RX IS (LUNRR DESCENT)

FIGURE :28 d RRNDCJM VI BRRT I ON SPECTRUM

LOCRTICJN 30

-o L fV'IS -t- 12E.$ P()tvSE -~----------------------------~------------~

N I

' N°0

2. 099'-! G-RMS I

X -~--------------~-------------+------------~ X C)

)-

I-

(f)

z W-Ob _J -~-------------~--------------~------------~ cr: a: 1-u u.J 0.... V)

2

5/24/71

** RLSEP ARRAY E/SP-l,F~RCING IN Z-RXIS JRN.1971 **

FIGURE 29 ~ TRANSMISSIBILITY

LeJCRTieJN

LMS l - Res PON~E-....... ~ _______ __,__ _______ -r··-----

C\J

... ; >-0 1-- ........ ~--...... en _Jco

r-...... CD COtn ......

... •a

2 3 l! 5 6 7 89 1 r:f 2 3 l! 5 6 7 89 FREQUENCY (HZ)

' 2 I

3 ~ ~ 6 7 89 ~ oli

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-(f)o ....... 0)

c.:> co r-

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w :::1' (J) ("()

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(J)

Page 99 5/24/71

** RLSEP ARRAY E/5P-1.F~RCING IN Z-RXIS JAN. 1971 **

FIGURE ~Cl b SINE RE5P~N5E

L~CATI~N 31

L/YlS

SPEC.

'

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0)

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r-CD

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FREQUENCY (HZ)

1"-J I ........... 0

ruo

Page 100 5/24/71

** RLSEP ARRAY E/SP-l.F~RCING IN Z-RXIS JRN.1971 *~

FIGURE 2Cfc.. RAND~M VIBRRTI~N SPECTRUM

L~CRTI~N 31

LM S

~ ~~-------------4--------------+-------------~ ~ C)

>-!--

1"1

b

rJ 2

5/24/71

RL5EP ARRAY E/SP\ 1. FCJRC I NG IN Z-AX I~ (LSG ~ LM5)

FIGURE .::

5/24/71

RLSEP ARA E/SP-1 (LSGJ , F~R IN Z -RX IS (LUN8R DESCENT J

FIGURE .2CJd RRNDOM VIBRRTI~N SPeCTRUM

LCJCRTI~N 31

LMS

~, ) +./ ')

11. 8319 G-RMSl I I

~0 I X -~--------------+---------------r-------------~ X

CJ

>-...._ ....... (f)

z W-o'o _j

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1 01 2 3 4 5 6 7 8 9 1 cf 2 3 L! 5 6 7 8 9 1 cf 2 FREQUENCY lHZ)

5/24/71

** RLSEP ARRAY E/SP-l.F~RCING IN Y-RXJS JRN.1971 M

F I G U R E 30 Q TRANS M I 5 S I B I L I T Y

L~CATI~N 32

LS P

·--------·----+-----1- - __ j I I I

I I I

I

- ,,---

Page 104 5/24/71

** RLSEP ARRAY E/SP-l,FCRCING IN Y-RXIS JAN. 1971 **

FIGURE 3D b SINE RESPeJNSE

...-f cn--...,=1~

CD-! r--j

~j ~~ (Y)~ ru~

L~CATI(jN 32

l-S p ----r-------------- -------·--·-r·----------- ------------,

I I i I i I

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3 4 56 789 0'-!

PC~ge 105 5/24/71

MM RLSEP ARRAY E/SP-l.F~RCING IN Y-RXIS JAN. 1971 M

F I GUAE 36 c ARND~M VI BRAT I CJN SPECTRUM

L~CRTI~N 32

-o L s P y- r~sfY" Vl~·e

N :r: ........ (\Jb0

~ ~~---------------+-------------~

D

>-1--en z

I I I

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Page 106 5/24/71

RL5EP RRR E/SP-1 (LSG) , FC!R IN Y-RX IS tLUNRR DESCENT J

FIGURE. 3cd RRNO~M VIBRRTI~N SPECTRUM

L~CRTICJN 32

Lsp

3. SG97 G--RMS

X ~~--------------+---------------~-------------4 X 0

'I-

t-1--t

if)

z W-O'o

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w 0..... (/)

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I

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5/24/71

** ALSEP ARRAY E/SP-1, F~RC I NG IN X-AXIS (PSEJ ~~

FIGURE 3l Q TRANSMISSIBILITY

L~CATI~N 6 C\1 0

0')

co r-w ll)

:::1'

(T)

N

->-0 t-- ........ t-1 0')

_Jco r-

-w cnll) t-1

(J)::3' (J) t-1

(T)

L

Pe1ge 108 5/24/71

~oE ALSEP ARRAY E/SP-1, F~RC I NG IN X-AX I 5 (PSEJ ;~(~

FIGURE 31 b SINE RESP~NSE

L~CATI~N 6

P'>e K- t?":'~ eor--J",c ~~--------------~----------~--~-------------~

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cf 2 3 L! 5 6 789 FREQUENCY CHZJ

5/24/71

** ALSEP ARRAY E/SP-1, FCJRC I NG IN X-AXIS CPSEJ *~

FIGURE 31C RANO~M VIBRATI~N SPECTRUM

L~CATIC!N 6 lA 1

X I ('" /) ,. ,-· fh',f:

I 3. 0573 G-RMS i

I

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>-t-....... (f)

z w-ob _J ~~----------~--~--------------;-------------~ a: a: t-u w CL (f)

2

I I

.I

5/24/71

RLSEP ARR E/SP-1 (PSEJ • FCJR IN X-AXIS (LUNAR DESCENT)

FIGURE 3ld RANDOM VIBRRTICJN SPECTRUM

N ::r: 'Q C\JC)

LCJCATICJN 6

X ~~--------------+-------X

C)

1. 6500 G-RMS I

i I

-j ~ I ~ i

>-t-

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1.

Db ~~--------------~--------------~-------------_J

~ I ~ :

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I

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Page lll 5/24/71

~~ ALSEP ARRAY E/SP-l,F~RCING IN Y-RXISfPSEJ NN

FIGURE ?·~ Cl TRANSMISSIBILITY

LCJCATICJN 22 No ...... en (1:)

r-CD

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(f)

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101 2 2 s ll s s 1as1 03 2 3 4 s s 1ss1 ott FREQUENCY CHZJ

5/24/71

** ALSEP ARRAY E/SP-1,F~ACING IN Y-AXISCPSEJ **

1-1-

·-1-

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1-

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FIGURE 3,;) b SINE RESPCJNSE

LCJCRTICIN 22

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FREQUENCY (HZJ

5/24/71

~~ ALSEP ARRAY E/SP-l,F~ACING IN Y-RXISCPSEJ ~~

N I

'c No

FIGURE AAND~M VIBRATI~N SPECTRUM

L~CATICIN 22 ) v,

Y 1-< ~~ P6l\J 'S'f:

2. 6932 G-RMS

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FREQUENCY CHZl

I

3 4 5 678S~o·

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Page 114 5/24/71

RLSEP RRR E/SP-1 CPSEJ. FOR IN I-AXIS (LUNAR DESCENTJ

N ::r: .......... 0

No X X

C)

>-t-1--i

en z

_J

a: a: t-u w Q_

en

.-4

FIGURE 3~d RANDOM VIBRATION SPECTRUM

LClCATieJN

P5E

'x I \

22

2. 0033 G-RMS j·

I

I

I --t-·

5/24/71

** RLSEP ARRAY E/SP-1. FCJRC I NG IN Z-RX IS (PSEJ ~oE

FIGURE 33Q.. TRANSMISSIBILITY

LCJCRTICJN 24 Z-.J t

No PS' E -l. -- t? .::: ':, ('0 L.J :__ ~--~~--------------~--------------~--------------~ 0) co r--CD

lf)

:::1'

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lf) -

5/24/71

** ALSEP ARRAY E/SP-1, F~RC I NG IN l-AX IS (PSEJ **

)-)---)-

)-

·-,_

N ,_

1-1---1-

lt) 1-

·-w (J)(Y") 1-

z 0 a_C\1 1-

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FIGURE

en Wo a::O 'I ~ ,_

1---1-

0)

co r-(D

lt) 1-

·-::Jf ,_

1-

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:::;., '!

5/24/71

** ALSEP ARRAY E/SP-1, FCJRC I NG IN Z-AX IS (PSEJ *~

FIGURE :33C. RANDCJM VI BRAT I CJN SPECTRUM If; /1

LCJCATICJN

-0 :;l- {(. es PON S'E ~~--------------~-------------~------------~

2. 3939 G-RMS

N I '--o (\JQ

::te~ ::!(

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__J

cr: a: (I 'X t- • u I . w . } Q_ J • en \ a: (\I I • I Wb ~~ D Q_

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~~~~--~~~~~~~~~~~~~-.--.-~lrrrri 2 3 !!56789JQ3

FREQUENCY CHZJ

5/24/71

RLSEP RRR E/SP-1 (PSE). FCJR IN Z-AXIS (LUNAR DESCENT)

N I

'0 (\JQ

FIGURE 33d RANOCJM VIBRATICJN SPECTRUM

LCJCATION 21.!

1. 7327 G-RMS

~ -~--------------+---------------~------------~ ~ C)

>-t--U) z:

_j

cr: a: t-u w CL U) I

l ~-~---: ·----t--·__j

/\ I I ' ! . ' • I

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rJ 2 3 14 56789 3 4 ~ 6 789~ a~ FREQUENCY CHl)

ATM 989

Array E Subpack I Dynamic Analysis 119

PAGE OF

DATE 5/24/71

6. 0 APPENDIX

Figures A-1 Through A-8

...-,.,._-: .......... ~~ ...... ~ ....... , .... _ ... t ............................ - ............ ~ .... \ .............. '• .. ---·

4 () ~ l. 1 1 / l !.0 1 2.~) • 6! ; ! 11 2 ~ 1.0

Page 120 5/24/71

-· ·- ·::- ··2.; -~ .·;;:7eti9-··-·;c;·1rrc;T--:z:n,·~~ l. 0 43 30 1.0 44 :n 1. 0 45 .. -~' 1. 0 4t: 27 0.557·

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(t.f'C, VE/PSitJN)

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10 9 1.0 10 25 -.555685 11 9 1.0 11 25 -.059843 12 10 1.0 12 25 .286052 13 11 1.0 13 25 .0209664 14 12 1.0 15 13 1. 0 16 14 1. 0 p 15 1.0 18 16 1.0 19 17 1.0 20 18 1.0 21 19 1.0 22 2C 1.0 23 21 1.0 24 3 1.0 25 12 1.0

26 13 1.0 27 22 1.0 28 23 1.0 29 24 1.0 30 22 1.0 31 25 1.0 32 2fJ 1.0 33 2l 1.0 3 ... 25 .557 3:.i 281.0 36 28 1.0 37 28 1. 0 38 29 1.0 39 30 1.0

.CC57376

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39 39

Pa.ge 123 5/24/71

1 10.6~ZZD noo.Sh36D•OL-.3tlOO cn-.650lD-Ol-.19~30-0lO.l6ZOD oo-.6~460-0Z 1 ~O.lA370•020ol817D-Ol-.?92lD-OZ-.l5920-02-.4~93D-030.lll80 00-.8322D-Ol 1 15-.1~180 00 2 20·. 97410 CC'C • 89430-0l- o4446fl-Cl0. 31940-02-.64080-02-. !l7050-020 .8302fl-C 3 2 9-.11520-Cl-.20210 000.34880-01C.4679D-020.37050-0l0.48900-0l-.37750 00 3 30.997AD oo-.2~3on oo-.747en-cz-;719IO oo0.4751D-ol-.1188D-Olo.azo9o-oz 3 100.4672D-Ol-.1Cl8D-Ol-.89820-02-.l304D 000.33730 00-.28480 00 4 40.44560 oo-.5eszo-cto.9303D-Ol-.2?71D-02o.5qs8n-oz-.95820-0l-.46l70-o2

. 4 ll-.84~6D-03-.[895D-020.43680-02-.l74ID-010.9126D-01 5 50.5C40D 00-.5E4B0-C40.1777D-01-.32l~D-Ol-.2346D 00-.12360-02-.20040-02 5 l20.1748D-02-.f682D-C20oll550-0l0.6523D-02 6 60.12800 01-.38140-010.66200-02-.30560 OO-.l5200-010o45230-0lO.lllOO 00 6 13ct.43280 ()0-.1C770 01-.12410-01 7 70.51860 00-.47670-Cl-.65740-C1-.12090-01-.4428D-010.10420 000.13860 00 7 14-.27COD 00-.70530-CZ 8 80.76880 00-.13590-Cl0.28100-020.1272D-Ol-.50620-0l-.18llO-Ol0.3500D-Ol 8 150.12030-02 9 90.10050 Ol-.4~43D-020o955CD-Cl-.20H7D-Ol-.1677D-010.143ZD 000.48820-01

10 100.43520 00-.13190 0~·.5335D-C1-.3373D 000.14280 100.44180-0l 11 110.12980 01-.20r90 00-.62110-01-.349QD-010.3788D-01 12 120.69410 oco.~577D-Ol-.33f4D o0o.2412o-o1 13 130.16830 01-.138~0 C1-o57850 00 14 140.204~0 010.25390 co 15 150.77710 co 16 l60.5332D-Ol-.103C0-010.5221D-C10.11850-0Z-.27380-03-.2701D-020ol4~50-03 16 23-.8093D-030.22540-CZ-.5161D-OlO.l6410-0l 17 170.3449D-Ol-.1218D-Ol0.484~0-02-.4055D-03-.1812D-020.31500-030.15270-02 11 24-.6r,sqo-ozo.z3a5o-020.37C5r.-o2 18 l80.7447D-010.35C80-C~-.5735D-02-.108RD-020.1302D-02-.27250-02-.7113D-Ol 18 250.85330-020.19340-r.l 19 190.50640-010.38290-02-.78630-0Z-.39090-020.44560-03-.38480-010.17690-0l 19 26-.14800-01 20 200.7305D-Ol-.1f74D-Cl0ol030D-Cl-.1059D-010.11830-010.57030-02-.5410D-01 21 210.13330 00-.1C7CO 000.5725D-020.98R~0-020.1017D-Ol-.33900-0l 22 nO.l416D OC-. 2C'CID-03- ·• 38520-C20. 858"i0-030. 33220-02 23 2~0.3134D-OlO.lr93D-Ol-.1234D-C1-.3531D-02 24 240.14090 00-.48370-01-.27630-01 25 250.11820 co-.~434D-01 26 260.l299n oo 27 27 .166631 -.Cl27412 -.0341232 0.0206591 28 28 .lt6631 .C206594 -.0341227 29 29 .162758 -.011490t 30 30 .162755 31 31 .729693 -.257414 • C485912 • 0485912 32 32 .729693 .04E5912 .C485912 33 33 .967728 -.3382~~

34 3~ 36 37 38 39

34 .967728 35.237997 36 .113067 37.22(:474. 38.1371

array e subpack i dynamic analysis #80...19d random vibration spectrum (lunar descent), xmtr...

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