1 1

MINUTES

Tenth Apollo Lunar Surface Program

Interface Meeting

September 7, 1967

The tenth of a series of Apollo Lunar Surface Program Interface meetings

was held at The Bendix Aerospace System Division, Ann Arbor, Michigan,

September 7, 1967.

Mr. Joe Clayton, Bendix ALSEP Program Director, opened the meeting and

welcomed all to Bendix. Mr. Small, Manager, Lunar Surface Project

Office then introduced Dr. C. O. Alley of the University of Maryland

as the PI for the Lunar Laser Ranging Retro-Refl<i:ctor experiment.

Each organization (PI's, contractors, etc.) gave a status report which

included the following:

a. Overall schedule status

b. Accomplishments to date

c. Forecasted accomplishments

d. Problems

The enclosed agenda shows the organizational elements and subject

material presented. Presentation material used is attached. Pertinent

points discussed are briefly summarized below:

a. The schedule presented by Dr. Snyder on the SWS shows that

the Qual Model will marginally support the required delivery. However,

due to conflicts with OGO calibration, it probably will be shipped

uncalibrated. Dr. Snyder introduced Mr. Bob White who is replacing

Mr. Gary Walker as project engineer at Jet Propulsion Laboratories.

b. Mr. Herb Cross, speaking for Dr. Sonett, stated that the LSM

design is now frozen. The Proto type unit has been delivered. The

Qual unit does not support the System Qual at Bendix.

c. The PSE schedule was presented as supporting the System Qual.

2

However, a recently discovered problem could cause some delay. Dr. Latham

requested and was given Mr. Phil Claskey, at Teledyne, as a point of

contact for Test Program Status. LGO plans to have continuous coverage

during all testing at Teledyne and Bendix.

d. The SIDE schedule was reported as approximately 3 weeks late

to support the System Qual at Bendix. This is due'basically to long

calibration time.

e. The CCGE gauge is currently undergoing mount revision. However

can still support system testing.

f. Dr. C. Alley gave a brief description of the Lunar Laser Ranging

Experiment including the scientific objectives. It was pointed out by

Mr. Small that this experiment has not been assigned to a flight but

development and fabrication is geared to the f;rst Lunar landing mission.

g. Mr. Al Schorken presented the ALSEP Test Program Status and

briefly described the planned tour of Plant #2.

h. After the tour Mr. John Driscoll described the LM/ALSEP Inter­

face Design Summary and Mr. J. Burns presented the ALSEP Status.

i. An integrated lunar surface program schedule is enclosed.

The following action items resulted from the meeting:

B70907-0lM - MSC will provide clarir-lcation of ALSEP hardware nomencla­

ture by October 1, 1967.

Mr. Moke to each PI.

\ \

B70907-02S - ARC to provide impact to add survival heater to LSM by

October 1, 1967.

Mr. Cross to Mr. Moke.

B70907-03B - Bendix to provide plan for calibration of GFE/GSE by

September 21, 1967.

Mr. Clayton to Mr. Small.

~ -L ie/l ... ··( / J W. Small, Manager Lunar Surface Project Office

3

AGENTIA

APOLLO LUNAR SURFACE EXPERIMENTS PACKAGE

Interface Meeting

Bendix Aerospace Systems Division

Ann Arbor, Michigan

September 7, 1967

9:00 a.m. Welcome Mr. J. Clayton

9:05 Introduction Mr. J. Small

9:15 - 1:30 p.m. Organizational Status Reports:

Overall Schedule Status

Accomplishments To Date

Forecasted Accom-plishments

Problems

9:15 SWS Dr. C. Snyder

9:30 LSM Dr. C. Sonett

9:45 PSE Dr. G. Latham

10:00 SIDE Dr. J. Freeman

10:15 CCGE Dr. F. Johnson

10:30 CPLEE Dr. B. O'Brien

10:45 ASE Dr. R. Kovach

11:00 HFE Dr. M. Langseth

11:15 LRR Dr. C. Alley

11:30 DRILL Mr. M. Goldman

11:45 RTG Mr. W. Remini

12:00 Noon

12:30 p.m.

1:30

3:00

3:30

4:00

4:30

ALSEP Test Program Status

Lunch

Review of ALSEP Plant #2 Operations (Prototype Testing, Manufacturing, Human Factor, etc.)

ALSEP Status

LM/ALSEP Interface Design Summary

Question Period

Adjourn

2

Mr. A. Schorken

Mr. J. Clayton

Mr. J. Driscoll

ATENDEES

L. Tiffany Bendix

A. Ketler General Electric

J. Burns Bendix

G. Chang Bellcomm, Inc.

J. McDowell Bendix

R. Shay Bendix

R. Kovach Stanford University

G. Latham Columbia University

P. Maloney NASA-MSC

J. Langford NASA-MSC

R. Moke NASA-MSC

J. Clayton Bendix

J. Small NASA-MSC

C. Schorken Bendix

J. Kenney NASA-MSC at Bendix

J. Sanders NASA-MSC

A. Collins Bendix

R. Swain Teledyne

R. Schmidt Bendix

P. Hickson Bellcomm, Inc.

J. Zill NASA-MSC

W. Sandstrom Marshall Labs.

W. Smith Rice University

J. Stenning Bendix

E. Van Valkenburg Bendix

2

J. Musslewhite Rice University

Ao Robinson Bendix

Jo Dye Bendix

G. Walker Jet Propulsion Laboratory

W. Collier Jet Propulsion Laboratory

B. White Jet Propulsion Laboratory

J. Redd NASA-MSC

D. Sherwood NASA-MSC

J. Harris NASA-MSC

M. Yates Bellcomm, Inc.

H. Rudolph, Jr. NASA-KSC

W. Johnson Bendix

C. Ahlstrom Bendix

J. Grayson NASA-MSC

Lo Fekete Grumman Aircraft Engineering Corp.

T. Newman Grumman Aircraft Engineering Corp.

Lo Lewis Bendix

C. McClenny NASA-MSC

K. McDermott Columbia University

H. Miller Bendix

H. Greider NASA-MSC

L. Paine Bendix

A. Stephenson NASA-MSC

J. Sulester NASA-MSC

R. Longmire NASA-MSC

R. Irwin NASA-MSC

w. Dunaway

C. Vaughn

w. Durrett

J. Driscoll

G. Young

E. Davin

H. Culver

Ko Schaver

F. Pallon

J. Lewko

w. Collier

M. Goldman

w. Remini

J. Carroll

Dr. Jo Freeman

Dr. C. Alley

Dr. B. O'Brien

H. Cross

Dr. C. Snyder

NASA-MSC

NASA-MSC

NASA-KSC

Grumman Aircraft Engineering Corp.

Teledyne

NASA Headquarters

Goddard Space Flight Center

Bend ix/ GSFC

Bendix/ GSFC

Bendix

Jet Propulsion Laboratory

Martin-Marietta Corporation

NASA-MSC

3

Gra.duate Research Center of the Southwest

Rice University

University of Maryland

Rice University

Ames Research Center

Jet Propulsion Laboratory

SN 5 GIU/Ja 1

SN 6

UNIT

QU/\L SPAr:~

SN 7 ruel:r 1

..

... • SCHEDULE AND STATUS

7[;~:J CO!\'iPLETE STNLFD FO::! n::-l\~~:~C)~::.c",:-!

f!!i',S[QU~~~T TO 1 :"; ::::-. r'(~:/.,,',:' ~ i! T() ~. ~ i·:;~c-cr(!.':) ;;D

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1. CHOICE OF HIGH-VOLTAGE RESISTOR

2. SENSOR MOUNTING

3. STReNGTH OF HIGH-VOLTAGE STANDOFFS

. ..

4. BREAKAGE OF FIU\MENTS FOR DUST COVER REMOVAL

5. REJECilON OF POWER TR.\NSFORMERS FOR fLIGHT UNITS

..

I

1. CO/v\PLETE QUALIFICATION OF SENSOR

2. INSTITUTE FAILURE REPORTING TO MSC

3. APPROVE CALIBRATION PROCEDURE

4. EVALUATE RESULTS OF PROTO~G TEST AND TAKE APPROPRIATE ACTION

5. II\WLEMENT SOLUTIONS TO H!Grl-VOLTAGE A~CI~]G PR03LEM

1. CALtORATION PROCEDURE GENERATED

2. MECHANICAL SHIUCTU.RE DESIGN AND INTEf;;:I\CE FINALIZED

3. INSTRUMENT QUAL TESTING SUCCESSFULLY CON~?LETr:D, EXCEPT FOR SENSOR

4. FAILURE REPORTING SYSTEM WITHIN EOS AND JPL INSTITUTED

5 .. SENSOR STIMULATOR TESTED AND APPROVED .

6. THERMAL-MECHANICAL SIMULATION UNIT CONSTRUCTED AND DELIVERED

7. SWS NO.4 DELIVERED TO JPL

8. FIRST ARTICLE CONfiGURATION INSPECTION COf.:2LEn:f:', INCLUDING

A. FREEZr; OF DEl.IVEPv~GLI: DOCUMENTS

B. FREEZE OF HARDWARE DESIGI'--l, INS~'i:CnOh! TECHNIQUES, AND FAGRICA1'ION DETAILS

C. DrAWING F[~2tZr:

COPIES OF MR. H. CROSS'S SLIDES

WERE NOT AVAILABLE AT PRESS TIME

,

PSE PRODUCTION SCHEDULE

-AUG SEPT OCT NOV DEC 67

1

68 JAN

8111 5 WKS 9115 SN-l l:r--------:-O

~ = ALEX SCHEDULE DATES o = SLI P DATES FROM TELEDYNE 8/30

SN - 2

SN - 3

SN - 4

SN - 5

SN - 6

SN - 7

9/8 6 WKS 10/16 l:r--- -------0

10/6 11/10 Lr- _.2 yJ1S~ - --<>

11110 11115 ~-O

11117 12111 ~_~_WK_S_ -<>

12 /13 12 115 Ob:

12/22 1 '7 ~---O

~~22-2700

PSE ACCOMPLISHMENTS · I

• LGO TESTS (MODEL EM- 2)

• OPERATION THROUGH 26 JULY /

• LIGHTNING DAMAGE 26 JULY

• RETURNED TO TELEDYNE • RETA I N AS REFERENCE MODEL

• DVT UNI T TO lGO AFTER TESTS • LONG TERM. FUNCTIONAL. TESTS

4422-·2703

· ..

PSE ACCOMPLISHMENTS . III

• DVT • SCHEDULED TO RESUME VvEEK OF 4 SEPT • DE LA Y C AU SED BY

• PERIOD ADJUSTMENT • FLEXU.RE SPRING RATE

• DRIVE SCREW PASSIVIZATION • RECOATED

• CAG I NG MECHANI SM • REVISIONS MADE, PASSES LEAK TEST

• NOISE EVALUATION • UN I T USE DIN TE 5 T

• LPZ CLAMSHELL INSTALLATION • LATEST DES I GN 4422-2701

PSE ACCOMPLISHMENTS . II • PROTO

• RETURNED TO' BxA 1 AUG • NEW BELLOWS • NEW LPZ CLAMSHELL • NOISE SURPRESSION MODS

• PRE-INTEGRATION TESTS 2-3 AUG. • I NTEGRATION TESTS 4 AUG.

• SENSOR EXC I TER MOD I F I ED TO • ELIMINATE CAL SIGNAL LOADING • I NTEGRATI ON TESTS REPEATED 31 AUG

4422-2702

CPLEE QUALIFICATION AND FLIGHT MODEL SCHEDULE

SEPT OCT NOV DEC JAN FEB ~~AR

QUAL MODEL A QUAL MODEL SPARE ~ ~

ALSEP ARRAY B QUAL TEST I

i FLI GHT MODEL # 1 ~

I FLIGHT MODEL #2 (SPARE) ~ ,

FLI GHT MODEL #3 I

FLI G HT MOD EL #4

APR rv,AY JUN JU L ,

.

, ~ i ,

I

~ ~

~ ~

4422-2709

CPlEE PROTOTYPE SCHEDULE

1967 . 1968

SEPT OCT NOV DEC JAN FEB MAR

ASSEMBLY AND FUNCTIONAL TEST .

ACCEPTANCE TEST AT BRl -C~I BRATION FU CTI ONAl TEST WI TH ARRA Y C -PROTOTYPE ARRAY B SYSTEM TESTS ..

EXPERIMENT INTEGRATION . ..

P ROTOTY PE D VT , 4422- 2708

CPlEE DESIGN VERIFICATION TEST MODEL

AUG SEPT OCT NOV

DVT MODEL DEL~VERED BY BRL 8-15 •

CALI BRATI ON LAB CHECKOUT AT RICE _8-19, I

RETEST AT BRL .8-24

PERFORMANCE TEST AT BxA 8- 31 EMI TEST

. MAGNETI C PROPERTI ES TEST • CALI BRATION AT RI CE PIA AT BxA • ACCELERATION ,

SHOCK -VI BRATION THE R rv, A L -V A C U U r..,

1

4422- 2707

MAJOR ACCOMPLISHMENTS CPLEE

• DESIGN VERIFICATION TEST MODEL DELIVERtD BY BRL

• FUNCTIONAL TEST PERFORMED AT RICE .

CALI BRATI ON LA B. ,. DVT TESTS STARTED AT BxA • ALL SUBASSEMBLIES FABRICATED FOR CPLEE

PROTOTYPE MODEL • 70 o/f) OF QUAL MODEL SU BASSEMBLI ES

FABRICATED. ' ,4422-:- 2704

. ~ . .

CPLEE PROBLEMS

• RADIAL CRACKS IN SWAGED TERMINALS

• BLACK COATI NGS ON PHYS I CAL ANALYZER . BAFFLES AND APERTURES

• VACUUM TEST FAC ILl TI ES AT BRL

• COMPLETION OF I N-PROCESS AND SU 8-ASSEMBLY TEST SPEC I F I CATIONS

~~22- 2705

ACTIVE SEISMIC EXPERIMENT

SCHEDULE STATUS • OVERALL SCHEDULE-NO CHANGE • SUB-CONTRACTOR SLI P (TRANSMITIER PROBLEM)

ACCOMPLI SHMENTS ------• SUCCESSFUL RECEIVER QUAL TEST • GRENADE BALLAST REMOVAL CHANGE

3 GRENADES, TOTAL O. 6.LBS • GLA/GLA TIS REWORK COMPLETED

-MODIFIED GLA -MODIFIED TEST SET VERIFIED BY INERT -NEW CABLES GLA TEST - NEW PROCEDURES

• 50S RESUMED GRENADE TESTI NG 4422-2716

, . . ,

•

ACTIVE SEISMIC EXPERIMENT ".

•

ACCOMPLI SHMENTS (CONTI NUED)

• BENDIX BOARD OF INQUIRY COMPLETED

~ ASE I NVESTI GATI ON t CONCURRENCE - ASE CORRECTIVE STEPS f

• WSTF PROGRAM -INITIAL SUBSYSTEM TESTS COMPLETED .. - SYSTEM NOI SE CHECK AT WSTF

• ~ CDR AT GEOTECH - SIN LEVEL CHANGE IMPLEMENTED - QUAL UNIT COMPLETED ACCEPTANCE TESTS

• DVT PLAN COMPLETED 4422-2717

ACTIVE SEISMIC EXPERIMENT

PROBLEMS

• TRANSM I TTER LONG TERM FREQ.D. RIFT - CDC TEST/EXPERI MENTAL MODEL

PROGRAM - BERRY RECEI VER STU DY

• I NCll NOMETER -NEW ANGLE SENSOR EVALUATION -RANGE ACCURACY ANALYSIS

• TEST EQU I PMENT 4422-2718

• •

ASE TRANSMITTER SCHEDULE

CDC TASKS MONTHS AUG.

FREQ. DR I FT TESTS BU I LD PROTOTYPE RE-QUAL. PROGRAM ~ CDR

FLI GHT DELI VER I ES 1ST FLI GHT GLA

NEED DATE

•

•

SEPT OCT.

-•

NOV.

4 1,":,') '"'7'"' 1 ..... 4...4.-4-1 L

A S E / W S T F PRO GRAM

SKS SEPT. 6 7 8 9 1112 1314 1516 18 19 202122 2325 27 28

SYSTEM C/O (BxA) SHIP ASE TO WSTF INS PECT & CALI B. SETU P & cIa TRR MEETI NG PROCEDURE DRY RUNS CHARGE FI RINGS THUMPER FI RING GLAs AT WSTF GLA cIa GLA FIRINGS

4422-2720

• i

.

ACTIVE SEISMIC EXPERIMENT

FUTU RE EFFORTS

• RESOLVE TRANSM lITER FREQ. D RI FT PRO.BLEM . - ~ CDR

- NEW QUAL • CONDUCT RECEIVER CDR • COMPLETE & DELI VER WSTF GLAs • CONDUCT WSTF PROGRAM

- COMPLETE SYSTEM TEST AT BxA - TRR MEETI NG - CONDUCT TESTS AT WSTF 4422-2719

H.F.E. DELIVERABLE HARDWARE SCHEDULE

1967 1968

SEPT OCT NOV DEC JAN FEB MAR APR rv'AY JUNE JULY

DVT . • • HARD\VARE DELI VER I ES

PROTOTYPE • • • • GU L TON DEL.

QUAL. • • • • A. D. LI TTLE DEL.

QUAL. SPARE • . ~ • BEND I X DEL.

FLT. • • • FLT. • • • FLT. • • • ALSEP PROTO "B" TESTS

.1422-2710

H.F.E. DESIGN VERIFICATION TEST SCHEDULE

r OCT I NOV DEC I J 2 9 16 23 30 Q 13 20 ?7 4 11 13 25 3 1

1 I I I I I 1 1

A V A I LAB I LIT Y 0 F H ~ E D V T ~y 10 DEL ~

TEST PROCEDURES COf\IPLETE ~

TEST FIXTURES Cor\IPLETE ~

PERFORT\,ANCE TEST - .

E~ \ I • HU ~\1 I D I TY • PERFORr,\ANCE

SHOCK -~)E R F 0 Rr,IA NCE -VIBRATION • PERFOR~.'A!~(F

T H f R ',~, A L V A r I I:J ~,' 1

4422-2711

ACCOMPLISHMENTS TO DATE

1. ENGINEERING MODEL 2 ELECTRONICS SHIPPED FROM GULTON TO A. D. LITILE ON 8/4/67.

2. DVT (FORMER PROTO) MODEL ELECTRONICS SHI PPED FROM GULTON TO A. D. LITILE ON 8/17'/67:

3. THE QUAL 41 1 (FORMER QUAL 412) IS UNDER·GOI NG ELECTRICAL CHECKOUT AT GULTON.

4. ALL OF THE PROBE AND PROBE PACKAGE DRAWINGS HAVE BEEN APPROVED AT A. D. LITTLE.

5. E2TRAINING SIMULATOR AT A.D. LITILE IS BEING N

UPDATED TO LATEST DRAWINGS CONFIGURATION. ~ N

6. THE CONTENTS OF THE ACCEPTANCE DATA PACKAGE ~ TO BE USED BY A. D. LITILE HAS BEEN APPROVED.· ~

ACCOMPLISHMENTS TO DATE (CONT.]

7. THE PROBES ARE BEl NG I NTEGRATED WITH THE ENG I NEER I NG MODEL ELECTRONI CS.

8. THE DVT PROBE (FORMER PROTOTYPE) HAVE BEEN ACCEPTED AT A. D. LITTLE. THEY ARE BEl NG I NTE­GRATED WITH THE ELECTRONIC AT A. D. LITTLE.

9. FLI GHT MODEL PROBE BEl NG ASSEMBLED. 10. THERMAL SIMULATOR CDR HAS BEEr4 HELD DU R-

ING JULY. ALL ACTION ITEMS HAVE BEEN COMPLETED. 11. TEST PLAN FOR DVT AT BENDIX COMPLETED AND ISSUED 12. APOLLO LUNAR SURFACE DR I LL I NTERFACE CONTROL

SPECIFICATION HAS BEEN SIGNED OFF BY MARTIN, BxA AND MSC. 4422-271:

HFE MAJOR PROBLEMS ,

I. THE DVT MODEL HAD TO BE RETURNED TO GULTON TO REMOVE METAL CHI PS \JVH' CH

,/

GOT INTO ELECTRONI CS. 2. SOME DIFFICULTY IS BEING EXPERIENCED

BY A. D. LITTLE IN SATI SFYI NG THE RE­QU I REME~~TS OF NPC 200-4 , N SOLDER INC THE PROBE LEADS TO THE ELECTRONI CS.

3. THE THERMAL SI/'v~ULATOR SHIPPING DATE HAS SLI PPED TWO WEEKS.

~~22-2715

t , • •

HFE MAJOR FORECASTED ACCOMPLISHMENTS

1. THE DVT MODEL SHOULD BE TESTED AT A. D. LITTLE AND INTEGRATED AT BENDIX DURING THE MONTH OF OCTOBER.

2. THE PROTOTYPE SHOULD BE SHI PPED FROM A. D. LITTLE DURI NG OCTOBER.

3. THE LABORATORY AND THERMAL VACUUM SIMULATORS SHOULD BE I N ACCEPTANCE TESTING DURING SEPTEMBER AND EARLY OCTOBER.

4. DESIGN VERIFICATION TESTING SHOULD START DURING OCTOBER. 4422-271

COPIES OF DR. Co ALLEY'S SLIDES

WERE NOT AVAILABLE AT PRESS TIME

Go-ahead

Preliminary design review

Critical design review

Simulator, structure

Development model

Development test program

Simulator, therm/mech

Simulator, mass

EMI test model

Qualification test model No. 1 No. 2

Training model No. 1 No. 2 Spares

Qualification test program

Flight model No. 1 No. 2 No.3 Spares

GSE: Battery chargers (6) Pressurization units (3)

Complete interface definition (ALSEP contractor)

ALSD/ ALSRC Interface First article config insp

Status as of 8-31-67

MAJOR MILESTONE SCHEDULE--ALSD

CY 1966 CY 1967 CY 1968

S 0 N J) J F M A M J J AI S 0 N D J F M A M J J A

... 26 +bontractlexeLteA 11!10-~6 - 13 18 I I I

Y + Delta PDR

281 4

• .Freli~ '1

vBtry

Pwr H( ~I t __ ~~ 5 l;-in. config~ation and NASA action items

Accessories i ~ ~ I I I 6 ""3 Meter rock model

+

fTiTiT ~ 17 ~ • Reconfiguration to NASA train/devel. model

~l po 11

5 III '1 '1

8

~ 7 8 -Q-

Modify V

¥ 1 E~ 22 ~ 1~7 19

Jf '1 ~ k.

-&- ~~ 6 1(2)

¢' IIF tool rework from Bendix -- ~I/F tool from Bendix ~~ ... -0.-- .() -- 01-__ -- ~Interface spec

1 : I I ~ Ir Interface spec

~ I [ \l

.0 Incentive item

DPR 3-10 Appendix II

S 0 N D

E = Early

DELIVERABLE GLFC HARDWARE

ENGINEERING UNITS -

· HARDWARE AVAILABILITY

H5 - PRIME CASK

· QUALIflCATlON PER PRIME UNITS

· SPARE WILL BE SPARE FOR ALL PRIME UNITS

· COMPLETION THROUGH AEC STAGE INSPECTION BY 4/15/68

H6 AND H7 - 1G AND 1/6G TRAINING MOCKUPS

· NON GRAPHITE MATERIALS - WOOD/MAGNESIUM

· WEIGHT/CG SIMULATION

• SIZE AND SHAPE SIMULATION

· OPERATING BREECH LOCK AND SPLINE MECHANISMS

· NO 7HERMAL OR LOAD REQUIREMENTS

· COMPLETION SET FOR 10/1/67

PRIME UNITS - 4 FLIGHT PLUS ONE SPARE

· TWO UNITS THROUGH STAGE INSPECTION BY 4/15/68

· THREE UNITS THROUGH STAGE INSPECTION BY 6/30/68

37

1.0

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..... . . ... _-",---

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500

1050 f CE-'CEPT EVE'N STR' N 6tHOO. e,,)

'I' ""1' iOOO 5000 iC¥)OO

EL~PSEO TcM~ ~ HOURS

so, 000

PROCEDURE -----

1. INCOMING INSPECTION TEST, PCU TEST CHASSIS

A. VISUAL INSPECTION ,

B. ELECTRICAL BENCH TEST Wllll SIMtlLATED PCU

C. ELECTRICAL BENCH TEST wrlll BENDIX PCU

2. ELECTRICAL CHECKOUT, PCU TEST CHASSIS WIm IPU TEST CONSOLE

3. RTC-PCU INTEGRATION TEST

R'TG CHARACTERl5"TIC T~£o~e"lcAL MIN\MUM

au } o

00.

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,.. ~----~----~----~~----~----~----~~--~~----'ev

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8f:NO'X PCU CHARACTER,sTtC A-r !, V IN P V -r

(CONVERT£~ ANO Re6ULA"TO R.)

A

i 1 ; , ~

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0" e 111/$/"

RTr. - PCI r INTE(;RATION TEST PROGRAM

PURPOSE

1. CHECK COMPATIBILITY OF PCU AND RTG DESIGNS.

2. DETERMINE PERFORMANCE CHARACTERISTICS OF PCU-RTG SYSTEM UNDER SELECTED CONDITIONS

RID TEST RESI'LTS c.

NON VENTED VENTED

1 2 3 4 5

PHASE I - 418 HOCRS IN T/V + .47.. + .4% + .3% - - - + .15%

(3024) (2896) (2958) (2977) (3007)

CALIBRATION - CYCLING + .005% + .09% + .05% + .01% + .015%

PHASE II - 200 HOllRS IN T/V + ,10% ± .05', + .05% + .05% + .05%

(2992) (2987) (3041) (3012) (2972)

PROBLEMS:

SOLUTION:

RESULTS:

CONCLUSIONS:

RID STATUS

MOI~) lURE AB!JORPllON AND SLOW DRY OUT DUE TO SMALL CRACKS IN HERMEn C SEAL YI ELDING LOW INSULATlON RESl STANCE AND DR I IT

Vf:NTING WITH POROUS PLUGS

TESTING OF TWO VENTED AND THREE NON VENTED UNITS

PHASE 1 - T/V TES1ING BEFORE AMBIENT CALIBRATIONS

PHASE I [ - T Iv TESII NG AFrER AMBlENT CALIBRATIONS

ACCEPTANCE TESTlNG OF PRIME UNITS

DRY OUT RATES ARE ACCELERATED AND UNlTS ARE NOW CONSISTENTLY STABLE

HERMETIC SEAL IS NOT NECESSARY

UNITS MUST BE IND1VIDUALLY CALIBRATED TO EACH GENERATOR INSTALLATION

1967 1968 JULY AUG. SEPT. OCT. NOV. DEC. I JAN. FEB. MARCH APRIL MAY JUNE

2, B H Ill! 111m 113 J4 119 I- 11. .lI! 48~1 U Q M 4S • 41 tel 4151 51 5111 I I 4 • • J • I II n II II 14 15 II 11t1 II a II II n H 21 21 ISYSTEMS ENG' G

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~t.~LJ 1 }(UiTtJU~J\Ct: l(ldd~/t\.·mp~

1 REQM -I S S pi::e P !If f' ISAFETY WIU Tt;UPS ~,. ,

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., , 'Cl r:: aI B " int, struct ~ ,.

DESIGN f l1~ht rc !t'ast" ~ -, ,. p ~,.

I MANUFACTURING I , ,

I~ ~ ~ P IP. F ..J pi FS"" p~,

I Nl t.KNAL ~ l.l<lJ~ IURI 1 ., " .. I' " .. " ."

ENG G GRAPH! n: 'f/ I (.i , I G '1-

QUAI CASKS ., ,. tz t'~ f'1 ~ :s- 1" 'p

n,lGHI CASKS 1oIj, ~4 ,,. , ., ~ [ "I ., ,.,

MOCKUPS " ~

~,

SHIP 'G CONTAINEK~ ~,. , F 'I' M )'

n:s 1 IENGI'NEERING -- I",

1-~ALl.fl.CA nON -~(.ll)[~LE

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RTG CH,4RAC.,.ERtS..,.lC T~~O~t"l'AL MAJ.IMUM

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4. 5 CI..JG.QEN'T- AMP,!;

~

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AO~-+--~ __ ~ ____ ~ ____ -+ ____ ~~ ____ ~ ____ ~ ____ ~~ ____ ~ ____ ~ ____ ~~ ____ ~ __ 1200 ItIOO ~ooo ;)100 'l~OO »00 3f,OO ~

TOT~L AC.C.UM UL~TE.Q 'TEST ",ME

PROBLEMS: -.---.-

SOLlITION:

RESULT§.:

CONCLUSIONS:

RID STATUS

MOl~IURE AB!JORPILON AND SL~ DRY OlIT DUE TO SMALL CRACKS IN HERMEflC SEAL Y1ELDLNG LOW INSULATLON RESISTANCE AND DRU.,.

VENTING WITH POROUS PLUGS

TESTING OF TWO VENTED AND THREE NON VENTED UNITS

PHASE I - T/V TESltNG BEFORE AMBIENT CALIBRATIONS

PHASE II - T/V TESTING AITER AMBlENT CALIBRATIONS

ACCEPTANCE TESTING OF PRIME UNITS

lJRV OUT RATES ARE ACCELERATED AND UNlTS ARE N~ CONSISTENTLY STABLE

HERMETI C SEAL 1 S NOT NECESSARY

UNITS MUST BE INDIVIDUALLY CALIBRATED TO EACH GENERATOR INSTALLATION

RTIJ TF.S'l RFSi 'L 1'5 llOOor UN t TS

NON VENTED

1 2 3

PHASE I - 418 Hor~s IN T/V + .4'/, + .4% + .3/0 - - -(3024) (2896) (2958)

CALIBRATION - CYCLING + .005% + .09% + .05% - -

PHASE II - 200 HOURS IN T/V + .10% + .05/, + .05%

(2992) (2987) (3041)

VENTED

4

:t . 15;,

(2977)

+ .01%

+ .05%

(3012)

s

+ .15%

(3007)

+ .015%

+ .05%

(2972)

RTC; • PCII INTEcRATION TEST PROGRAM

PURPOSE

1. CHECK COMPATIBILITY OF PCU AND RTG DESIGNS.

2. DETERHINE PERFOR.~NCE CHARAC'I'ERISTICS OF PCU-RTG SYSTEM UNDER SELECTED CONDITIONS,

Co

BENOIJ( PCU CHARACTER,\STtC A'T i' V IN P V 'T

(CONVERTf ~ ANO ReGUlA'-O R.)

A

1 j

= , ~

~ ~ . t l I ~

"'" .., -' 70 0" e¥:s'"

"" I-... ~2 .,-

< ~

\!}

c(

~15 ..J

~

10

5 ..

~.J -l'-i'

RT6 CH~RAC"ER~S-rIC T~FO~~-r,CAL M AJ.1 M UM

Q • 1.505 W

~

...

W\ ~

~~ } ~

1lI

3 0

aU.

0

C

~----~1----~2~----~----~4------5~----~~----~7~--~80

R"TG CHAAA~'TER1.s"'IC TW£o~e"lc"L til IN\MUM

.... ~----~----~~----~----~------~-----7----~~----~ev

C J C ~;~/(,.1

1. INCOMING INSPECTION TEST. PCU TEST CHASSIS

A. VISUAL INSPECTlON

B. ELECTRICAL BENCH TEST Wlm SIMULATED PCU

C. ELECTRICAL BENCH TEST WITII BENDIX PCU

2. ELECTRICAL CHECKOUT, PCU TEST CHASSIS WI1li IPU TEST CONSOLE

3. RTG-PCU INTEGRATION TEST

, ./ )

DELIVERABLE GLFC HARDWARE

ENG1NEERING UNITS -

· HARDWARE AVAILABILITY

M5 - PRIME CASK

· QUALIFICATION PER PRIME UNITS

· SPARE WILL BE SPARE FOR ALL PRIME UNITS

· COMPLETION THROUGH AtC STAGE INSPECTION IY 4/15/68

M6 AND M7 - IG AND 1/6G TRAINING MOCKUPS

· NON GRAPHITE MATERIALS - WOOD/MAGNESIUM

· WEIGHT/CG SIMULATION

• SIZE AND SHAPE SIMULATION

• OPERATING BREECH LOCK AND SPLINE MECHANISMS

.. NO 7HERMAL OR LOAD REQUIREMENTS

· COMPLETION SET FOR 10/1/67

PRIME UNITS - 4 FLIGHT PLUS ONE SPARE

· 'NO UNITS THROUGH STAGE I NSPEC'!I ON BY 4/15/68

• THREE UNITS THROUGH STAGE INSPECTION BY 6/30/68

1.0

,~

.8

--

,6

~MMARV 10 COutaLE MOOULE DATA

~. . . ... --",,~-

., .

_--& __ ....... --=i~O_5~0--r· _F_<. All .!a1' R, NG S ) 1050 f CE"~EPT EVE'N

STR' N~""OD, err)

I I , I"~ «I IIIII

.500 1000 5000 tC¥>OO

ELAPSED T.ME ,..., HOURS

....

I

so, 000

1967 1968 JULY AUG. SEPT. OCT. NOV. DEC. JAN. FEB. MARCH APRIL MAY JUNE

2J2I ,21 [a III Jl lm J4 II! I. n_ a .~I a Q ~ 4S • 41 411 .. 51 51 [52 I I I • • • J I I II 1111 III. 15 II n II II 121 11122 II M a • S' STEMS ENG'G j ISJ .NUIX INTERFACE

pads/tll:mos REQM lS SPt::C p lSAFETY WRI rt;ut's ~V'

mGl .~ .. ING -.NAl ", '~ ,. IAn: ~

Jl.taohltc O~ ,. , 'C ~ [CIl l rw

lot struct ,,. DESIGN

fl12.ht rCh~a8t" Go , r 1.1 ~,.

!MANUFACTURING I~ • :it IP IE f ~ P' ~ F S' p~

.INfERNAL ~lKUll URI I=. ., • I'tI [, ,r I'f " "I' ENG G GRAPH! n .~ I, G 11... QUAI ASKS .. " IZ f~ f''1 f S- f ''-'FLIGIff CASKS ~~ ~7

,,. " ~, ~

,. ,,. MOCKUPS " " SHIP'G CONTAINE/{~ " F 11= MS'

n:Sl .ENGLNEERING .QUA.Ll-fliATI ON. AUJ::PTArfCE ~t:uz.c -n3P.

- -

~- '-

pev TEST STATIIS

A, PLANS COMPLETED

B. SCHEDULE

o RTG/PCU INTEGRATION TEST PROGRAM

o INCOMING INSPECTION TEST

o ELECTRICAL CHECKOUT. PCU TEST CHASSIS

8/31

8/31

INSTALLED IN IPU TEST CONSOLE 8/31

o RTG/PCU UnEGRATION TEST 9/8

o ACCEPTANCE AND COMPATIBILITY TESTS BEGIN SEPTEMBER 11

o INTEGRATION TEST WITH MOD 8B BEGIN SEPTEMBER 18

1.0

,~

~J .8

.... -. 7

,6

~MMA"V 10 . CO~LE MODULE DATA

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

• F' t.OS'O • F (All ~'R\NaS)

--~-----P--~--~-1050 f CE"~EPT E"E'N

I I

soo

STR ft·" (!I MOD. e" J

I I , , , t I

5000

"- HOURS

I I I

tcpoo

MOD 5

Pe~s. '13.0 W J"Ott lu..,"'1l. N\~~1 ~\SOO "T ... _, '4 V 1_ ....... VOLT"C.E P~~~." 70.8 w ~OQ lVN"R C#I>.'( w W ,J.Wrv. ~ ... .

~--~Llf£ r(~l 'N VKIJUM

C.AAt.65 O~ POWER SuPPLY

J,

A lVNAR. NI<."T (l) lUN~ OAY

o A

AO~~--~--+-----~------~----~----~~----~----~~----~----~------~----~----:l000 l100 ~eoo »00 .-..00 ~ TOTAL Atc..uM Vl~TE.t> TEST ",ME

THERMAL VACUUM TEST

• FU LLY DEPLOYED ALSEP

• LU NAR SURFACE S HROU D (- 300 F, +278 )

• I NFRA-RED SOLAR S I MULATI'ON

• 200 ENVI RONMENT PARAMETERS

• NO'RMAL ALSEP H/K DATA

• S I MULA TO R B A C K U P 4422-2734

r •

EXPERIMENT D.V.T. TESTS

• DETAIL PLANNING BEING FINALIZED

• CPLEE E. M. 'I. AND MAGNETI C PROPERTI ES TEST PROCEDURES COMPLETE

• CPLEE E. M. I. TEST

• CPLEE MAGNETIC PROPERTIES TEST

4422-2735

PROTOTYPE INTEGRATION "A" CONFIGURATION AUGUST SEPTEMBER

30

I S I DE I NTEG I 31

SOLAR WINO INTEGRA TI ON

4422-2727

1 PSE I NTEGRATI ON

I I I I I I I I I I I I

5 LSM INTEGRA TI ON

6 7

,CROSS TALK TESTI

7 10 INTEGRATED SYSTEMS TESTS

11 18 CENTRAL STATION­& SYSTE~' E~'I

) PROTOTYPE ENVIRONMENTAL TESTING

"A" CONFIGURATION SEPTEMBER

MASS ~OPS I (SUBPAC 1 & 2) I

...

21 -29 I VI BRATlON' I (SU BPAC 1 & 2 ALL AXES) I

I I , I I I I I

OCTOBER

2 MAG PROPS (STOWED)

5 12 MAGNETI C PROPERTI ES (DEPLOYED)

13 20 THERMAL VACUUM . (DEPLOYED)

4422-2731

/-

QUAL TEST (PROGRAM SCHEDULE . "A" CONFIGURATION

SEPTEMBER

5 20 I I CENTRAL STATION INTEG.' 1

221

OCTOBER

I I I I

17 201

,;;.;.-.--....... I SUBPAC I I BUI LD UP I

23

NOVEMBER . -I

I I I I I . 1

II ACCEPTANCE TEST PROGRAM

I I I I . I

DECEMBER

4 3!3'63

QUALI FI CA TI ON TES T PROG RAI\1

4422-2729

..

5

I C IS HARNESS I

I J

/

QUAL CIS INTEG. & EXP INTEG . . '

'. "A" CON FIG U RAT ION SEPTEMBER

7 15

IDA T A SUB S Y STEM I 18 20

Ip:c.u·l .. 21

t I I I I l I .

.~. :

OCTOBER

CIS INTERFACE . TESTS W STS I

22 25 I (SoI.O.E.1 I

o I 27 I 3

~I _P_o S_" E_" ~l 10

ISOLAR WINDt

10 16 CROSS TALK (ALL EXP INTEG)

4422-2730

I I

QUAL EXPERIMENT P.I.A & E.M.I "A" CONFIGURATION

12 13

(S.l.o.EPIAI 14

I

SEPTEMBER

19

s.l.o.E. EMI I 18 19

(P.S.E. p.I.A.1 20 25

I P. S. E. E. M. I. I 18 19

SOLAR WI ND P. I. A.

26 29

SOLAR WIND , E. M. I.

.. -. , J

PLANT 2 TOUR

• HUMAN FACTORS TES"T AREA

• MANUFACTU RI NG FAC I LI TI ES TOUR

ELECTRONICS FABRICATION CLEAN ROOM GSE FABRICATION POTTI NG AND ENCAPSULATION I N-PROCESS TEST

MECHANI CAL FABRICATION AREA 4422-2732

PLANT 2 TOUR

• TEST .. PRESENTATION QUAL TEST I N COMPONENTS LAB .PROTO SYSTEM TEST IN S·YSTEM TEST LAB ASE TEST I N EXPER I MENT TEST LAB . ,CPLE;E MAGNETIC PROPERTIES·

. TES·T I N SCREEN ROOM TOUR OF TtV AND VI BRATION TEST AREAS· PRESENTATION OF EQU I PMENT, PLANS AND TEST SET UP FOR PROTO TtV TESTS 4422-2733

I ~ JUL

I I

PROTOTYPE MODEL SCHEDULE "A" CONFIGURATION

. I 1967 AUG , SEP

"' , I

OCT

CENTRAL STATI ONI NTEG ; "&MECH. ASSY :

7118

EXPERIME~T . I NTEGRATI ON

811 '----..... , ...... -----~ I DESIGN VERIFICATION

7/31 ~ I I

TESTS

10 120'67 HAil CONFI GU RAT ION EX PER I ~\iENTS (ACTUA L DELI VER I ES)·

~-PASSIVE SEIS~'IC

~-SUPRATHER~iAL ION DETECTOR ~---SOLAR WI NO

..

9/1+- MA~GNETOMETER I J 4422-2723

I I

I

QUALIFICATION MODEL SCHEDULE "A" -CONFIGURATION

I 1967

AUG SEP . . . JUL OCT

I

COMPONENT FAB & ASSY

I I I

CENTRAL STATION INTEG&MECHASSY

EXPERIMENT I NTEGRATI ON

EXPERIMENT· DELIVERY

9'8 9'22 SIDE9!8 PSE 9flS SWS 91 IS LSM 9/22

•

NOV I.

ACCEPTANCE E~ au A L TE S T S

TO 3'8·'68

4422-2722

,

PROTOTYPE AND QUAL MODEL SCHEDULE "8" CONFIGURATION

JAN FEB \'AR

FAB & REFURBISH PROTO TO "B" ASSY CONFIGURATION

EXPERI\iENT DESIG~ VERIFICATIO~

EX PER I f\ iENT ...-.....-I ... NT_E C_' R_A_Tl_O_N ..a..-.TE_S_TS ____ ~ TO 5 17 oS

DELI VERY (REQUIRED) ..... _ ...

2 23 3 8 .

CO\1,PO~E\ T FAB tJ A)SY

~ ~

'IB '1 CONFIGURATION EXPERIf\iENTS REFURBISH OUAL \iODEL PASSIVE SEISMIC TQB CONFICJRATIO~

HEAT FLOW CHARGED PARTICLE COLD CATHODE GAUGE

EX PE R I ~\iE~T

EX PER I ~\iENT ....... .A-..1 N~IT ... EG_R_A T_I_()~ ..... ·

DELI VERY IREOUI RED)

4422-2725

PROTOTYPE AND QUAL MODEL SCHEDULE ftC"~ CONFIGURATION

1967 1968

I SEP I OCT I NOV I DEC JAN I FEB I MAR I APR I MAY I JUN I JUL I AUG I SEP

COMPONENT REFURBI SH PROTO

ASSY&TEST II A" TO "C"

FUNCT.

l::t. TESTS

ASE •

CPLEE

SUBSYSTEM QUALIFICATION OF ASE, ONLY

S'S MECH DES

USES PROTO "All PSE & S IDECCGE AND PROTO IIBII CPLEE

\l SUNSHIELD

ASE FAB & TEST TO

rOUALo B

lASE QUAL :\iISSION

..... --"...... Slr-.~ULATIO~

8 q TO q 20"

4422-2724

FLIGHT 1 MODEL SCHEDULE

1967 1968 NOV DEC JAN FEB r . MAR

COMPONENT FAB & ASSY CENTRAL STATION INTEG & MECH ASSY. .

EXPERIMENT

EXPER I MENT INTEG RATION

DELI VERY ACCEPT

(REQU I RED) TESTS 1/26 2'16 TO 4/19/68

4422-2726

1

PRESENTATION

TO

SEQ INTERFACE CONFERENCE

SE~mER 7, 1967

GRthylMAN AIRCRAFT ENGINEERING CORPORATION

A. LM FUEL CASK

1. Struts finalized and manufactured for 60 lb cask. Parts are presently available

and two assembled units can be made available for shipment to Bendix When required

for DVT.

2. Preliminary drawing showing ac~ess to cask in SLA with new thermal door (cCA586) is

available now. Loading operation will be somewhat more difficult and new installation

demonstration at KSC is suggested.

3. One temperature measurement (MCR 55OC) has been added to the LM Fuel Cask System.

This will be routed through the LM telemetry and will be able to record a Bendix

selected temperature from time of fuel element insertion to seconds prior to launch;

and would then give system temperatures whenever LM telemetry is on.

4. GAEC to redesign parts of LM thermal shield (secondary do~r) to withstand direct

view of caak.

5. 18 accelerometers on LM Fuel Cask recorded data during LTA 3 DR (LM6). Data will be

available (approx.) end of October.

3

B. SEQ SUBPACKAGES NOS. I & II (ALSEP) (CCA 586)

1. GAEC/Bendix Hard Point interrace drawing signed off on 7/26/67.

2. Mock-up proved over-all boom concept is OK but many corrections were required.

3. Retro-fit to 1M 4, 5 and 6.

4. + 15 - 25 lbs.

, '" ,

'-. ~

5. Installation checlt fixttu'cS and master tooling to be sent to Bendix on

6. i\LSEI'/LN Hitl1(U'o.vial Syste:;l Test Ih:: );Jophy.

A. CC»IPONENT TESTING . .

Qualify each member of ALSEP wi thdrawa.l mechanism for: Salt Fog, Vibration, Static

Load, Sand and Dust and Thermal Vacuum environment as r~quired.

B. STRUCTURAL TESTING

(a) Build Quad II Structure and vibrate for required mission levels. (Use ALSEP and RTG

Fuel Cask as GFE). These tests are anticipated to terminate 1/1/tJ3 •.

(b) Measure deflections of Quad II structure on LTA-3D or LTA-3DR for three (3) leg landing

conditions, and other reasonable worst case landing attitudes.

C. THERMAL VACUUM TESTING

(a) Update Quad II Structure (same unit as for structural testing) to deliver to:

(a) Chamber A or (b) Chamber' B .•. or (c) G.E or (d) Bendix

for functional, thermal vcr~fication of integrated mechanisms and possiblY the interfaces.

Alterna.te: Use GAEC T/V facilities and remote actuation of mechanisms.

D. Y!i....f, S TI::uLATI ON

GilliC roco:?r.l::mds that 1.J:SC conduct a simulation of access and deployment in the KC-135 Airplane.

(Ref. LTX-I:8o-65 da.ted 8/15/67).

r~OTE: Preliminary Test plan due 10/1/67.

5

C. SlIXPLE Ru"'TURN CmTAIHERS (SRC'S)

1. Uew NASA requirement will move SRC' s to a modularized container in the descent stage

out bound and return them in the ascent stage.

other items in this dIs container will be:

a) PLSS batteries

b) TV camera System (Including 100' TV cable)

c) ~O' dish cable

D. S'l'ILL CA1!'EFA PACKAGE

1. GAEC is currentl:¥" p:roposing to build this package (ECP /f11l4)

a) Itc::'lS "rill be s:)i't stol'red by cCJlpressing then in foam.

c) could serve n.s uti15_ty cout<1in8r.

ICD M:D IR'T l;U:,~BER MID TITLE

118-360-22101 1a SCmlT1FIC EQ.UIIMENT

MATERIALS COMPATAB11ITY

REQ.UIRE.lENTS _

11S-360-22101-1 ADDED 1UBECO AND EVER-

1UBE TO THE MATERIALS

LIST.

1IS-360- 22102 SCIElITIFIC Et;;:UIF1:lZlIT .MASS

FROERTIES.

118-360··22102-1 CC:·UII7D Fill·! COliTS

6 8IGN OFF

GilliC 8 & AD

10/21/65 10/21/65

4/13/67

10/21/65 10/21/65

12/21/65

CUR..~"sN1' EFFORT OR HE'SD FOR ACTION

GAEC IS CURRErIT1Y STUDYING THE ~'1E1G

AND BALAl'CE llIP11CATImlS OF LAmICH

ANY 1M UITHOUr SEQ..

ICD lum IBN Im:.IDEH AIJ) TITLE

LIS-360-22102

22102

22102

'·22102

2. LAUliCRED F & TCONT., SEQ.

CAMERA EXTRA FIlM CONT. MID

STILL CAI·1ERA CONT. IN LEM VS

CM.

3.. INCORroRATED CCA 1.83

4. LAUNCH STILL CAMERA IN 1M

VS CM. IlICORroRATE SCN /I 27b

5. REDUCED m. OF F & T.

6. PROVIDE FOR RTG (ccAl.83)

7. 2:{ Th. SRC

8. cCA498 (60 1b. CASK) 9. 40 1b. SRC

10. EFFECTIVITY

A. GZITEl.~AL UPDATE

B. GEI?:ZRAL tJPDATE AND MOD.

KIT DEFInITION.

LIS-360-22301 Ely[RO;:~:,.:r;l;'l'AL C01lDITIOI-JS IN-

DUCED BY THE I1-1 on THE STILL

CAMERA PACKAGE.

SIGN OFF ( '1 GAEC S & AD

7/1/ 66

6/7/66

7/1/ 66

8/9/66

1/10/67

1/19/67

4/15/67

5/2/ 67 6/1/67

9/11/ 67 9/15/67

10/21/65

8/25/66

DISAPPROVED

DISAPPROVED

DISAPPROVED

2/13/67

2/10/67

6/21/67

6/20/67 6/21/67

DISAPPROVED

10/15/67

LIS-360 .• 22301-1 GErr.:RAL UFDATII~G rE'CLUDIHG AN 4/20/66 12/13/66

UFDATED CABIn F?.2SSURZ (Vs)

CURRENT EFFORT OR NEED FOR ACTION

A N"Ell SECTIOH Fon CAl·rEB.."- co:n:E!ITS ,

BE m:::(UInED IF GAEC IS TO BUILD COl

TAINER.

ICD Arm IRN nl~T"sR Ai';D TITLE Gll.EC ~~~~~~~~~~-=-----------------;.-

SIGN OFF !I S & AD

LIS-360-22301-2 DEFIifES ENVIROK;·IENTS FOR

LAUriCH, BOOST AND TRANS­

LUNAR PHASES BECAUSE SCN .

276 REQU!RED CAr·rERA TO BE

CARRIED IN LEH (Vs) CM

LIS-360-22301-3 DEFIlED VEHICLE EFFECTIVITY

AS 111-4-15 (CCA575)

[.1S-360 -22301-A ADDED THE ENVIRONMENTAL

CRITERIA FOR THE LUNAR

ASCENT PHASE (cCA468) AND .

INCORPORATED IRN's NO 1, 2,--

3.

8/1/66 -~/1/66

3/18/67 6/21/67

11/15/67(EST) 12/15/67 (EST.)

L1S-360-22302 EUVIRO!~·OOITAL CONDITIONS IN- 10/21/65· 10/21/65

DUCED BY U1 ON THE SCIENTIFIC

E~UIP. IN THE DESCENT STAGE.

VEJUCLE EFFECTIVITY IJ.1-4 ArID

SUBSE~UEl'IT

L1S-360-22302-1 REVISE VIBRATION HORDING

L18-360-22302- 2 TEI TZFATURE CONDITIONS

LIS-360- 22302- 3 JI.DD2D 'I:=-'1·iP. TIME HISTORY

CURVE OF TITS SEQ BAY TO

leD.

7/1/ 66

11/2/66

8/25/66 .

ll/09/66

CURHErIT EFFORT OR NEED FOR ACTIon

VIBRATION SECTION WILL NEED UPDATI:

A RESULT OF THE LTA3 DR (LM6) AND }

(LIVE T/V RACKET FIRING) TESTING: I

THER.'fAI SECTION WILL NEED UPDATING

RESULT OF CCA586 (HAX DOOn:.9~ T!J

reD MID rRN rm:BER iU!]) TITLE

IJIS-36o-22303 ENVIRm~·:ENTAL conDITIONS IN­

DUCED BY LH ON THE LUNAR

SAMPLE RETURN CONTAINERS

L1S-360-22303-1 DEFIllES TEHPERATURE TIME

HISTORY CURVES OF 1M WALL

AND IM ASCENT ENGINE COVER

L1S-360-22303-2 CHANGE SPECnfEN TO SAMPLE

TO AGREE WITH LSP-360-11

LIS-360-2?,303-3 VEHICLE EFFECTIVITY

LM 4 ANS SUB.

LIS-360-22303-4 eCA 668-SRC's OUTEOUND

IN D/S

>:ilUl~ U.l!'.!!' '1 GAEC S & AD

12/21/65

/20/66 11/9/66

/1/66 9/1/ 66

Ll/15/67( est) 1/2/68 (Est.)

CT.lRt'lliNT EFFORT OR NEED FOR ACTIOn

NEH ENVIRm:OOlTAL corIDITImrs mLL

BE ADDED FOR Nmi· D/S SRC LOCATIOn

OUT BOUND.

IeD film IRt'I Nu:·ffirn AND TITm GAEC

".Ii,." ·.r ~. . '"., l" 1,IS-360- 22304 ENVIRor)MENTAL CONDITIONS 12/21/65

INDUCED BY ill ON SEQUENCE

CAHERA EXTRA FIUI CONTAINER.

LIS-360-22304-1 DEFnms A TEMPERATURE TIME 4/20/66

HIS'I'ORY CURVE OF THE IM CABIN

LIS-360-22304-2 DEFINES ~~IROM{KNTS FOR

LAUNCH AND BOOST AND TRAlIS­

LunAR (SCN 276)

LIS-360-22304-3 VEHICLE EFFECTIVITY

Lr:r4 AND SUB.

9/11/ 67

5/30/ 67

S & AD

12/21/65

11/09/66

10/11/67

6/21/67

CURRENT EFFORT OR NEED FOR ACTIO!l

DRAFT OF 304-2 CONPLETED BY 10/14,

IRN NOW BETh"G REVIEl'/ED IN HOUSE BY

GAEC. DELAY BE'TImN COMPLETION OF .. AND GAEC REVIEW DUE TO NAA FAILURE

SIGN OFF IRN 6043.

ICD AJ!D IRU N12,lBER AND TITJ..E

LIS-360-22305 ENVIRO~{&NTAL COrIDITIONS

INDUCED BY IN ON THE FILM

AND TAPE CONTAINER.

LIS~360-22305-1 DEFINES TEMPERATURE

TillE HISTORY CURVES OF IM

CABIN 'HALLS AND ASCENT

ENGINE COVER.

11S-360-22305-2 .DEFn1ES EIN1RCIi~,fE:NTS FOR

1AUNC'H AND BOOST MID TRANS-

1illIAR (SCH27b)

1,18-360-22305-3 VEHlcm EFFZCTIVITY

Iz,r!~ Alill SUll • .

11

SIGN OFF

GAEC S & AD ClffiHENT EFFORT OR NEED FOR ACTION'

12/21/65

4/20/66 11/9/66

10/1/66 11/21/66

5/12/ 67 6/21/67

SIGN OFF =1~CD~N~m~. ~I~m~~~m~-~I .. ~~r~on~~~r~~T~IT~LE~ ____________ ~G~EC

L1S-360-22402 EINIROr-:MEI1TAL CONSTRAINTS

IMFOSED BY IM ON THE 1M FUEL

CASK

LIS-360-22402-1 NEI-l T'rlERMAL AND VIBRATION

CRITERIA

LIS-360-22402-2 NEW VIBRATION RESULTS

LIS-360-22501 U~ ELECTRICAL POy!ER ALLO-

CATION AND COnSTRAINTS FOR THE

SCIENTIFIC EQUIPHENT (SEQ).

..

i ,

L18-360-22501-1 'GElffiRAL UPDATING INCLUDES .. .

CIIAl;GE OF LH I'imlIl'TAL VOLTAGE

fl.AUGE FROI4 24-33VDC TO 26-33

FRer J.,OOO HA'tTS 'IO 780 VlATTS

~0/20/66

~/2f3/67

~0/67 (Est).

';1.2/2l/66

11/16/66

DISAPPROVED

1l/67 (Est).

10/2l/65

12/13/66

CURFEIlT EFFORT OR NEED FO::t ~CTION

LTA 3 DR (IM6) VIBRATION RESULTS TO

INCORPORATED IN -2 IRN. NEW SURFAC

EMISSITIVITIES DuE TO CCA 586 WILL

ADDED LATER.

ACTIVE COOLING MAY ELD-rrNATE 48 HR

ASSOCIATION RE~UIREMENT.

A GFE D-lPEDAliCE SIMULATOR MAY BE

REQUIRED (NASA DECISION) FOR U{ 4

AND SUB "FEAT" TESTS •

... .) SIGN OFF 13

rCD AI']) IRN' Nl~:I3~:!.R~fJ..::.'.:.::::m~T=-I::::,;T::.::LE;:;:" ______ J--..::G:.:..AE:::::.:::.C ______ .::.S....:&;:,...:.AD=-___ ~ __ .....;C::.;UR=RENT=::......::E:;:F..:,FO-=.;.;.RT:.,.-::O:;.R:......::.NE:::E:::;D:..c.:FO..:..:.:R...:A..:,:C::T:.:;I..:::.ON:.:..-

LID-360-22502 :u.r tITRING ELEc'rmCAL

INTERFACE FOR SCIENTIFIC

EQ.UImENT

REMARKS - VEHICLE EFFECTIVITY LTA-1,

LTA-8, LM-4AND SUB. SIGm;n

OFF BY EPO MID GAEC AT

SEQ MEETING No.4. 502-1

ADD EFFECTIVITIES

L1S-360-22503 ETECTRICAL nrrE-~FACE BE-

Th'EZIT THE RA.DIOISOTOPE

Ttrr:;;::::,:O:;;:;LECTRIC GEllEI'J\TOR

(R'i.'G) Ci\SK SHIELD TEl,fP-

EPJ\'I'UIE TP!l~SDUCER A.I!D THE

EI v.c:nCLE.

12/21/65 12/21/65

9/15/67 10/15/67

ESI, LTA-1, LTA-8, LM4 and SUBQ.

EFFECTIVITIES WILL BE ADDED.

LM-3 CAN BE ADDED IF DESIRED

ADD LM-3.

9/15/67

DRAFT COPY AVAILABLE TODAY

ICD AIm IRIi ImmER AND TITLE

Lls-360-22700 DELIVERY, INSTALLATION AND

PRE-LA.uNCH SERVICING RE-

QUIREHENTS FOR LH SCIENTIFIC

EQ,UIFI.fKNT •

'i

LID-360-22704 SCIENTIFIC EQUIPMENT BAY

PRE-LA.lmCH ASSESSIBILITY

SIGN OFF GAEC

3 Mo. SUBQ.

TO REQ.UIRE-

MENT DEFIN­

ITION •.

If S & AD

10/1/67(Est.) 11/1/67 (Est.)

CURRBIIT EFFORT OR NEED FOR ACTION

SEQ REQUIREMENTS NOT YET DEFINED TC

GAEC - BEING RESOLVED TODAY.

.... BEING UPDATED DUE TO CCA586 AND MAY

REQUIRE REVISION TO PLANS FOR PRE-

LAUNCH INSTALLATION OF THE RTG Fl~

ELEMKNT. COPY IS AVAILABLE TODAY.

-.; SIGN OFFS j.)

;::I.:::.CD::.....:.A.::::.:.~n.....;I;:;..:I:.;;:\."1'.:..r ..:.:1'1:.;:;.'::.:.::n:;;;];;.:JR.:...:..:PJ.:.:.·ID::......:T:.;:I:.;:T~LE=-___ ~ ___ ::G .. :.:::\E:::.:C=--___ ---:-...:::-...::&~AD=--____ -+_..::.C:.:::UR~tRE~~IIT E?FORT OR IffiEO FOR ACTION

LID-360-28302 SPECIMEN RETURN CONTAINERS

STOHAGE (LM)

LI8-360- 22802-1 CHANGE NCI·fENCLATURE

LI8-360-22802-2 REDUCED CORNER RADIUS,

4.00 INCH CRITICAL DIMENSION

TO BE MEASURED FROM CENTER-

LINE OF PINS TO BOTT<l.f OF

CONTAINER, CHANGED TOLERANCE

OF SRC vlIDTH AND VERTICAL C.G

DUlElTSION.

LID-360-22803 SEQ,UENCE CAI·IERA EXTRA

FTLr.1 COiITAINER STOIIAGE

~. (LM).

LID-36:J-22803-1 CIIt\E;E cor~:,;n R'JJIUS OF

10/21/65

9/1/ 65

6/7/67

2/21./65

10/21/65

8/15/66

12/21./65

10/20/6 7(EST. )

A NEH IRlI- 3 vlILL BE EEQ,UIRED TO E:,{Pi

EXTERNAL EnVELOPE TO n;CLUDE IIDII

(PIANO TYPE) HUTGES. DHG rrr;;::DED FRC

NASA.

'.

THE CONTENTS OF THIS CONTAIUER (100 f

CABLE) HILL BE S'l'O~nD IN TEE mSCENT

STAGE HIT'rl TILE TV CA!':l~Rl\,AND A r;EH T

CONI;EC'l'OR \':1LL BE ADDED TO Tl[Z D/S.

(CCA 668).

16 SIGN OFF

IG.2.1.~:D-,1;!D' N1~_::.rJ.!U'~l) TITI~i.-________ --!,T~t'~C~ ___ -I-~S-,&~A~D ___ --+ __ -..,;C:....;:tm~l~::.:..S1<'::;;~l:...:lT~E;..;.F~FO.::..:R::..;;T=--=O;..;.R~I~::;;'·F:....:,D~F.::..:OR~A~C-=T.::.IO.::..:J:.:..I_

LID-360-22804 STILL CJ'..! ~ PACKAGE

STO~L\.GE (Uf)

ru:,~.:\nI\.s - VEHICLE EFFECTIVITY LH-4 AND

SUBSEQ,UENT. SIGNED OFF BY

EFO ArID GAEC AT SEQ, MEETING

NO.3

LID-360-22Bo4-1 DEFINES MAX. ALLOHED TOL.,.·· 0/19/66

ERAIICE IN DISTANCE BETIlEEN

THE PARALLEL HOUNTING RAILS

ON 1M ErTGllm' COVER FOR

CAHERA

LID-360-22804-A fu..""VISED TIITERFACE DUOOISIONS 3/24/67

/ TO HITROVE I~rrERCHANGE­

ABILITY, U,CORFORATED IRN# 1

ADD:SD 170T PERTAINING TO DRY

10/21/65 MIGHT HEED Im';'l rCD FOR IIITERFACE BE-

'l'HEEH cmrrAINER Aim COHTEnTS DUE TO

ECP 1114. (GllliC TO PROVIDE COlITAU;z)

ll/9/66

7/25/67

Fn~,! L1J't~~I,~CA;.;;;l;.;.::rr::.:::s;..:.. ______ { ______ ! .. ______ -!, _________________ _

LID-360-22805 FllH AFD TAPE CONTATIlliR 12/2l/65 12/21/65 NAA IS RZQUESTn;G THAT cm;TAnu.:H BE

S'.rO~TAGE (LU) MOVED TIIBOARD 5/16".

L18-360-22805-1 DELsms 4 of 'l'HE 6 Cj\,LFAJ'{ 11/9/66 .

leD AI::D IRN' a;;·:r!-:RS Arm TITLE

LID-360-22809 1>~OmITING OF 34 1b RTG FUEL

CASK TO THE 1M.

LID-360-22809A 1-~OUli'TIN'G OF 60 1b RTG CASK

TO THE IM

809-1 CHANGE TOLL.

809-2 CHA1;GE DATUM TOLLERAlrCE

LID-360-22810 scmmFIC EQUIFMENT

CONTAINERS STOWAGE MID

REr'{OVAL (LM DESCENT STAGE)

LID-360-22810A 1001 ALSEP I/F

LID-360-22810 1 DEFn1El) , C. Q.

- LID-360';'22810':'2 TOLERAnCE CHANGE

LID-360-22810-3 VERTICAL COLUMN CLEARANCE

4 CHA.!-IGE DEMS~

5 CHf.];GE DEMS.

6. CHANGES TABS on U1- 3

7 LTA-8 OnLY (DISAPPROVED)

8 APPLIES 810 TO LM-3 &

LTA8 O:IT..Y

I

SIGN OFF GAEC

7/15/66

9/15/67(EST) (SIillET 1)

5/18/ 67

6/2/67

10/21/65

9/15/66

10/21/65

6/7/66

4/27/66

7/25/67

17 S & AD

12/10/66

3/16/ 67 (SHEET 2)

6/21/67

6/27/67

10/21/65

10/5/66

10/21/65

10/5/66

1l/09/66

8/31/ 66

6/21/67

6/24/67

DISAPPROVED

7/26/ 67

"

CUR?.EliT EFFORT OR liSED FOR ACTION

nICORf-DRATIOII OF EEIIDIX DESIGN AS E

3 OF YriE INTERFACE. HARD FOr:NT nrr

FACE s/o AND PARTS IN STOCK TO 1M 7

SHEETS 1 & 3 ARE BEING UPDATED TO C

TO CCA 498 and 586.

THIS ICD APPLICABLE TO LTA-8 AND 1M

,ONLY (OLD INTERFACE PRIOR TQ CCA 58t

\,

SIGN orr leD A1ID IRN NlI4BER AlIJ) TI TLI GAF£ 8 a. AD CURR E :E1fI' FFORT OR HEED FOR AC'l'ION

,

/7/26/67

';'~I

LID-360-2f611 DIf AL8BP III'l'JmJ'ACB FOR 7/20/67 , IR'l'ERFACE MUST BE QUALIFIED 'f"daJUGI ,

RDmI RDI)'IAL (CCA 586) JOINTLY BY r:JAFC/NABA

LID-360-22812 III taSCa, ftAGZ 10/1/frr(EST) 1l/1/67(FJ.ff) WITHDRAW~ SYSTEM CURREBTLY UNDER

SCIZlf'rIFIC zqrrlMEllT WITR- DEVELOH4ENT.

DRAWAL BYS'l'DI (CCA 586)

(IUlICrICfiAL) ~ ---

LID-360-22813 I.M SCIDTrFIC E<JlIlMIft 1/';13/66 2/7/66 !

JI!LBC'rllICAL IIft'IRFACE

0CiW/l,"rt)R LOCATIOlf

-\

IeD AND IRN !\ru;..mER ArID TITLE

LID-360-22814 1M SCIENTIFIC EQUIP-

MENT ELECTRICAL CONNECT­

OR THERMAL DOOR (FUNCT­

IONAL)

METHOD OF ATTACRING

DOOR TBD.

19 SIGN OFF

GAEC S & AD

4/25/67 4/25/67

. . \ \ . \

\.

CURRENT EFFORT OR NEED FOR ACTION

ATTACHMENT MATERIAL (VELCRO) WAS

FLAMABLE AND NEW MATERIAL MUST

BE DEVELOPED.

. ...

~-" ,-

? ,\ (r" '( '-~t

-~'r-- -

--.. -... _ .. .-"-- ---",,",-- ~ -'-'~--

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MSC 2570-68

[,~to"'" J' Systems Division MASTER SCHEDULE rit1e REVISED PROGRAM

INO: H IRevision No:

ALSEP IIsS\'i;d On: I Upjated ,~n: , ••••• ,',.. Ann Arbor. Michigan

Incorporating CCP No. 49 - LM I/F ChanJ;(e " 7 27/67 ·~/·~

L 1'1' 7 "('~ i Item ,."." ~ .7V<.,. n JiJL It"'rf;r ' s :;:f~L"

.:>cr Nt:>v p-., .;:;;,.v /'-:<4 r~J" f'~' Z,,, e r , LI .... , ,~ '0 Z 3 /D n 1.-1 / p, It,., ., N I, lr z. , "" 11 , IO/7~<l411I'1V .. "rl&

1 LM IfF Desi~n Chan~es I- 'J)~F '" f Ie., ,,- C c '" ~I 1

2 Primary Structure ASBv 2 3 3

4 Sub Pack=e 2 Assv ,.

4

5 5 6 Sunshield As sernbly. 6 7 - 7 8 Sunshield Procurement I 8

9 9 10 Sunshield Assv Build up -...,. , 'f " t. '1 • ti° 11 11 12 12 13 13 14 !fAll Configuration 14 15 Prototype ,I, 15 16 C /S Integ & Mech Assv

. 16

17 7 18 Expt Integration '/1 Its 19 I 'f\. ,N7 19 20 Desie:n VeriL Tests 20 21 21 22 ,Qualification Model 22 23 Component Fab & Assv - 23 24 24 25 Struct. Fab & Assv 25 26 ~

A ~~ 26 27 C fS Integ & Mech Assv ~ i""'

~I -- 27

28 -"'xpt l-'lA !i!! 28 29 Exnt Integration III II!! II! , ~ 29 30 M ~~R. Vz 30 31 Accep Tests 31 32 It(, !I 1/1 ~, 32 33 Qual & SirrlUl Mission Tests 33 34 34 35 Struct Therrn Subsvs Oual r'J ,C" ~ 35 36 Struct E'ab &cAssv 36 37 37 38 Sunshield Ass Avail I 38 39 39 40 Subsystem Ass,v. & Chkout I=:'::~ 40 41 41 42 Struc,/Therm Qual Test

-42

43 43 44 44 45 45 Remarys I I Next Higher Schedule No Page

Other Test Mig Dept Mig Prog Engr I Prog Canl-I _,_ of 6

910-28C

ritle 1:-.10: )..I Revision No: [ .~?"" ] ~ystems D~~S~_ MASTER SCHEDULE REVISED ALSEP PROGRAM

Incorporating CCP No. 49 - LM I/F Change IIssue1 ~'ii UP;~l;:!?n: . , .. " .. ".. Ann Arbor, Michigan 7 27 67

L 1q(.,7 19'8 i

n Item .1lL. " ,o/-Jr ... ~"n.,~ ,.0:;-; ZO l !.N,g>~?of I ~""l~ ~9 y 1/ ~ ... L li!!t / ~ ......... n~ .... 1 ~~)'I, ... 7:S:';N, .,. ~~ e 7 I~ ~ a. 9 ~f. ~6 ~I

1 I!AII Configuration 1

2 Flight I 2 3 Component Fab & Assy 3 4 4

5 Sunshield Assy Avail In 5 6 6 7 C /S Intel!. & Mech Assy 7 8 8

9 Expt Integration 9 10 10 11 Acceot Tests 11 12 12 13 n, ;ve.v r .. ,,'-I 13 14 14 15 KSC Checkout SUODt 15 16 16 17 Flioh' 2 17 18 Comoonent Fab & Assv 18 19 19 20 Sunshield Assv Avail '3 20 21 21 22 C /S Integ & Mech Assy 22 23 23 24 Expt. Integration 24 25 25 26 Accept Tests 26 27 27 28 Deliverv rl J/ ;1 28 29 29 30 KSC Checkout Suppt 30 31 31 32 32 33 33 34 34 35 35 36 36 37 37 38 38 39 39 40 40 41 41 42 42 43 43 44 44 45 45 Rerna r!·· 5 I I / /Next Higher Schedule No Page

I Other I Test Mig Dept Mfg Prog Engr J Prog Con,I 'ZA of 6 970 2SC

ritle )/0:

H JRevision No:

[ ~/I"" ]S},"-~.nl.S_ Oivi"i.on MASTER SCHEDULE REVISED ALSEP PROGRAM ' •.... ,' .. Ann Arbor, Michigan Incorporating CCP No. 49 - LM I/F Change Issued On: I Up~~te~~On: 7/27/67 .31- 1

L 1~'8 i n Item SUL Ao~ SCP

n r:;; I" l(' 'jOt , .... })e'fi3 Zo Z7 e ',l.(., z. '" " .2.3 30 " 13

I "AI! Confip'uration I

2 Fliaht I 2

3 romnonent Fab " Assv 3

4 4

5 Sunshield Assy Avail 5

6 6

7 CIS Integ & lvfech Assv 7

8 8

9 Expt Inte2.ration 9 10 10

11 Accept Tests II

12 12 13 Delivery 13 14 14

15 KSC Chec kout SuppL 15 16 16 17 Flight 2 17 18 Component Fab & Assy 18 19 19 20 Sunshield Assv Ava ... : 20 21 21

22 CIS Integ & Mech As~y 22 23 23 24 Expt IntetZration 24 25 25 26 Acct'pt Tests 26 27 27 28 Deliverv 28 29 29 30 KSC Checkout Suppt 30 31 31 32 32 33 33 34 34 35 35 36 36 37 37 38 38 39 39 40 40 41 41 42 42 43 43 <H 44 45 45 i{c:ma,~ '- I I Next Higher Schedule No Page

Other Test Mfg Dept Mfg Prog Engr I Prog ConL..1 ze of 6 970_2BC

N ,

'"

( ~V' J!i}'~~~S_DjVj,.j()"---. .•• II •• ".. Ann Arbor, Michigan MASTER

L i n Item e

1 "Btl ConfiQ'uration 2 p

3 F:lert npsi pn 4 Mech Design

5 Jel, ·t Je,h

6 7 c;, '" Ass, Avail 8 9 R '{"rh' ,h "r" " flR!1

10 11 Exnt Tntppratinn 12 13 n .. oi Vpri{i ,ti '" Tpoto

14 15 Qualification Model 16 Component Fab & Assy 17 18 Sunshield Assv Avail 19 20 Refurb Qual S/S Struct 21 2.2 C S Intep & Mech Ass 23 24 Exot Intep'ration 25 26 Acceot Tests 27 28 Oual '" S;""'I Mi "i nn Tpsts 29 30 Fli.ht 3 31 Comnonent Fab '" Assv 32 33 Sunshi_In A"" Av,' 34 35 Struc' Fab & Assv 36 37 CIS Inte. & Mech Assv 38 39 Exnt Intep rati nn 40 Acr,'nt T_sts 41 42 Deliverv 43 44 KSr, r,j,,,rkn,,t ,C;"nn' 45 Remarl,.s

970 28C

SCHEDULE ritle

1/f,7 ?~"~, "LJI ""c,.-/J-2\' 8~Fu~f'~ " ~

I I I Other T Test

REVISED ALSEP PROGRAM INo: H IRevision ~o:

Incorporating CCP No. 49 - LM I/F Change lIS sued On: 7/27/67

IUp~~ed On: -.1/.,7

1'1(., V ,t''it1f ~(~I ,:r<.l~~, .y ~;;. Nt,oJ .~""'¥/J 1.?';L. 9 ,~~ I ~'1A&- .. , r' ~~ u. ,. 1'IV I

1 2 3 4 5 6

~I# 7 8 9 10 11 12

r" 13 14 15 16 17

S 18 19 20 2.1 2.2. 2.3 2.4 25

111: ~t. 2.6 2.7 2.8 29 30 31 32. 33 34 35 36 37 38 39

.... ""'l ~ 40 41 42 43 44 45

I Next Higher Schedule No Page

Mfg Dept Mfg Prog Engr I Prog con .. 1 .3A of....6..-

N , ;;::

[ ~t/ J ~Y-,,-I!,~S_~ivi.S~ ITitle MASTER SCHEDULE REVISED ALSEP PROGRAM t •••••• ' ,. Ann Arbor, Michigan Incorporating CCP No. 49 - LM l/FC hange

L }'/66 i Item :!<JL n A1Jc,. SsP O:::-r- 1\):>1/ 1>Sc,

e ~., Z.{. l- I' L3 J", ~ /.:1 Zc ,7 7 fI' /( IT • .("' I I' /!' L.l-~, "I l.p l7

1 11BI! Configuration 2 Prototype 3 Elect Desi~n 4 5 Elect Fab 6 7 Sunshield Assv Avail 8 9 Refurbl sh !Te T1 to "BII

10 II Expt Intee:ration 12 13 Desie:n Verification Tests 14 15 Qualification Model 16 Component Fab & Assy

17 18 Sunshield Assy Avail 19 20 Refurb Qll~l SIS Struet

21 22 C IS Inte~ & Mech Assv 23 24 Ex:et Integration 25 26 Accent Tests 27 28 Qual & Sirnul MissioD Tests 'I'}"", 'L~ 29 30 Flipht 3 31 COn1:Q.,QDent Fab & Assy 32 33 Sunshield Ass Avail 34 35 Strnct Fab ~ Assv 36 37 CIS Inte~ & Mech Assv 38 39 Exnt Inteo ration 40 Accpnt T sts -,-41 42 Del·ver f ) , 43 44 K.~r rh >rk~nt S,onn 45 H.emark , I I Next

Other Test Mfg Dept Mfg Prog Engr I Prog Cor." 970_28C

:--Jo: H JRevision No:

Iss~/~7~6:7 I Updt:ed ,9r -$1-,

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45

Higher Schedule No Page

~S of 6

tv , ::;

l'~ ] _Systems Division ---c •••••• ",. Ann Arbor, Michigan MASTER

t Item e 1 'Coo C ,r; "0

~ Prototvoe 3 Elec Desi~n 4 5 !':Ier Fab & Test 6 7 Refurbish "A" to "COO 8 9 AS!':/!':xo' Funct. Tests

10 11 ",vot .<;"

12 13 r.PJ.!':E nVT 14 15 He' 1"10= nVT 16 17 ASE DVT 18 19 Qualification Model 20 ASE Fab & Test 21 Mech Design

22 Sunshield Assv Avail 23 24 ASE Qual Test 2! 26 ASE Siroul Mission 27 28 Fli~ht 4 2' rn~n"',ent Fab & Assv 30 31 <:;, Assv Ava 32

13. Struct Fab & Assv _3i 35 r. .'5 Tnteo Merh A"v 36 37 EXDt Intonation 38 39 Accent Tests

'40 41 Deliverv 42 42 Ksr rhMknnt Snnnt 44 4' Rerna d· s

970_28C

SCHEDULE rit1e

ll:f~z'd frU~(" 9=~,~ "7 c:t;-r:,

I 1 I Other 1 Test

REVISED ALSEP PROGRAM 1;';0: 1-1 r ,vi,ion:--io:

Incorporating CCP No, 49 - LM IfF Change IIss~i~7~6~ I Upd~~'J~.~': {.a

/Vol! , .. oJ, ~~ :(" /3:e. / ~~':';; /1.1:-., ,7,7;" "~'I' 'a,..

I I

4 IS ,6 17 8 9-10 1

12

114 15 16 i 7 18 ,9 - 20 21

77 22. Z3

2!

27 i8 i9 130

'f 131 132

34

36 37' 38 39 .. 0 41 4, 4, 44

J ,45

I I Next Higher Schedule No Page

Mig Dept Mig Prog Engr I Prog Coml If A of 6

N , ::x;

[.~y J ~YSle~S ~!"iSi-,,-,,-_ MASTER SCHEDULE /Title REVISED ALSEP PROGRAM

, •••••• T,'. Ann Arbor, Michigan Incorporating CCP No. 49 - LM IIF Change

L I'{ (8 i n Item :r\,l" f\tlcr ~p O:T 'No.1 DoC __ e '1'.l." z.. 1(, U o'/, 13)., Z7"~ ii II~S;<I 8 /f2ll "" /J'o Z7

I "e" Confi2uration 2 Prototvoe 3 Elec Design 4 5 Eler Fab ~ Test 6 7 Refurbish "A" to "c" 8 9 ASE IExnt Funct. Tests

10 II Fvnt ~. , <

12 13 CPLEE DVT 14 15 Heat Flow DVT 16 17 ASE DVT IS 19 Qualification Model 20 ASE Fab & Test 21 22 Sunshield ASBV Avail 23 24 ASE Qual Test 1000 -25 26 ASE Simul Mission ~I ..... I. 27 28 Fli~ht 4 29 Comoonent Fab & Assv 30 31 Sunshield Assv Avail 32 33 Struct Fab & Assv 34 35 r. S Intea \A'ech Assv ......... 36 37 EXDt Inte!:!ration 38 39 Accent Tests 40 41 Deliverv I oIh 42 43 KSr: r:heckont Sunnt 44 45 Remarl ... s T I I Next

Other Test Mfg Dept Mfg Prog Engr I Frog Cont..I 970 2SC

I~o: H IRe vision :-.J'o:

IIss~i:d~n: '7 27 67

I Up 'Y,ted ,9n: ,11-~

I 2 3 4 5 6 7 8 9 10 II 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 ~7 38 39 40 41 42 43 44 45

Higher Schedule No Page

48 of 6

tv ,

( ~ J Systems Division ' •••••• t, •• AnnArbor,Michigan MASTER SCHEDULE

L i n Item J"UI.. Pll.lc.-e 7 ,1/&., '1-" <# " 18,r I 1 Inert Models 2 Structural Model F 3 LM-3 IlF 4 5 LM-4 JiF 6 7 Therm/Mech Sirnul D-l 8 9 Therm/Mech Sirnul D-2

10 LM.J r/F 11 12 LM.4.I1E 13 14 Trainer Dev Model E-2 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 Remary.s Dates shown are MSC need dates as defined 7/27/67. I BxA schedule will be developed.

I 970 2SC

ITitle

rtf b 7 I SisI' OCT"

P /(1.1. l.' " 11'91.0~' J

~I [)

1 Other I Test

l'<o: Revision No: REVISED ALSEP PROGRAM Incorporating CCP No. 49 - LM I/F Change ps~n~/~~: Up~ate1 ~n: ,,3 • 1

\ij<o( ,.f,~I{~, I ~fr ~, 'f " ~~ z. q ff~~ ,~?Ih , , ~. J I. ~\v,t , 7 .::r"AJ ,j-<

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1 2

I~ I ,7 3 4

1./: L~ , 5 6

il ,A 7 8 9

I ./, ~j 10 11

,3 I ~ 12 13

o /II , 14

n"" 11>1 I> 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45

I I Next Higher Schedule No Page

Mfg Dept Mfg Prog Engr I Prog Con,,1 S of-'-

N , N o

[,~ J Systems Division --". II ••• ' ,. Ann Arbor, Michigan MASTER SCHEDULE

L i Item Ju'- ,<9</6-n

7 /jlLI ~t ~ II 1i'\t.S"" I e 1 Receipt of Experiments 2 Prototype flAil Coniie: 3 PSE ,g I

4 STDE 7~

5 SWS • .iI!!1UA 6 T.S 7 Proto "B" Conii, 8 C;C;GE 9 HFF.

10 rPTF.F 11 = r r. 12 ,"'" 13 r>, ' ,

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