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Qualification Status List ALSEP Array A2 Configuration
NO.
ATM 986
REV. NO.
PAGE I OF 27
DATE 5 March 1971
In compliance with the requirements of NASA contract NAS 9-5829, this document provides a Qualification Status List (QSL) for use as Section 3 of the ALSEP Array A2 Acceptance Data Package (ADP\.
As of the date of publication, the information herein rdlects the status of qualification following the systems level tests which have been completed on the ALSEP Array D system configuration. The ALSEP Failure Analysis Reports which are possible constraints to the close out o£ qualification status are discussed in Section 1. 2.
As of the date of publication, the information hp,·ein reflects the status of the Array A2 Qualificationr
There are four major changes which distinguish the Array AZ experiment package: substitution of a Bendix transmitter, a new solid state timer (RSST), re-design of the MDX, and the addition of the HFE to SP 2.
Prepared by: '/;}d., !}'. T. Baker ALSEP Reliability
R . db A b !~~ ev1ewe y:_J:.::_~~~~~~~~~,·· pproved y: __ .d'-__ ,,. __ 4 _____ _
Group Engineer ALSEP Reliability
S. J. Ellison Manager A L_S EP Reliability
Qualification Status List ALSEP Array A2 Configuration
NO.
ATM-986
PAGE 2
REV. MO.
OF
DATE 5 March 1971
CONTENTS
1. 0 INTRODUCTION
1. 1 HARDWARE LIST FOR ARRAY A-2
1. 2 OUTSTANDING FAILURE ANALYSIS REPORTS
2, 0 HARDWARE CHANGES, QUAL SA, SB TO ARRAY A -2 CONFIGURATION 12
3. 0 QUALIFICATION TEST HISTORY 24
3. 1 QUALIFICATION TEST HISTORY
3. I. 1 3. 1. 2 3. I. 3
BxA Transmitters Dual 9 0 Channel Multiplexer Converters Resettable Solid State Timer (RSST)
3. 2 SUBPACKAGE #2 ASSEMBLY
3. 2. 1 Heat Flow Experiment (HFE)
4. 0 QUAL A2 TEST REPORT LIST
APPENDIX A QSL SHEET COMPARISON CRITERIA
APPENDIX B QUALIFICATION STATUS LIST SHEETS
24
24 24 24
24
24
26
A-1
B-1
Reference Section
3. 1
3. 1. 1 3. I. 2
3. 1. 3
3. 2
3. 2. 1
ALSEP Array A2 QSL Data Sheets
CONTENTS (Cont'd)
SUBPACKAGE II! SP f/1, Antvnna Assembly Central Station Compon<·nts FiltPr Diplex<•r Diplexcr Switch Command Receiver Com.mand Decoder Data Processor Transmitter 90 Channel Multiplexer Power Distribution Unit Power Conditioning Unit C/S Timer (RSST) Passive Seismic Experiment PSE Sensor Assembly PSE C/S Electronics Shroud, Thermal Control PSE Gnomon Assembly
Solar Wind Experiment (SW) Lunar Seismic Magnatomett•r (LSM)
SUBPACKAGE //2 RTG Assembly RTG Shorting Plug ALHT PSE Leveling Stool Heat Flow Experiment (HFE) Suprathermal Ion Detection Experiment (SIDE)
NO.
ATM 986
PAGE 3
DATE
Shed
Bl B2 (B3-B12) B3 B4 B5 B6 B7 B8 B9 BlO Bll
REV. NO.
OF
Bl2 (Bl3-Bl6) Bl3 B14 Bl5 Bl6 Bl7 Bl8
Bl9 B20 B21 B22 B23 B24 B25
Qualification Status List ALSEP Array AZ Configuration
NO.
ATM 986
PAGE 4
REV. NO.
OF
DATE 5 March 1971
l. 0 INTRODUCTION
In compliance with NASA Contract NASA 9-5829 requirements, this document provides a Qualification Status List (QSL) for use as part of the ALSEP Flight 2A Acceptance Data Package.
Because of the similarity of this Array to previously qualified arrays, complete system qualification was not required. Those new components, which were identified at the FTRR/FACI for Subpack I on 27-28 October, 1970, as being qualified on a component qualification level are as follows:
(1) 90 channel multiplexer (2) BxA transmitter (3 \ RSST Timer
The FTRR/FACI held at Bendix on 16 December 1970 dictated that requalification rationale of the HFE SN 6 would be accomplished by successful completion of HFE SN 2 qualification on Array D subpack 2 qualification. The ALSEP Array D Subpackage 2 QAR Minutes, 9721-276, state that HFE is considered to have passed qualification testing.
Changes to Array A2 hardware previously qualified by the ALSEP Qual SA, SB, and SC Program are reviewed in Section 2. 0, and other comments concerning qualification by similarity are provided in Section 3. 0.
l. 1 HARDWARE LIST FOR FLIGHT 2A/ARRAY A-2
The following is a hardware list for the Flight 2A Array A-2 configuration that was reviewed at the FTRR as the basis for establishing the hardware qualified on an individual basis versus configuration items considered qualified by Qual SA, Qual SB, and/or Qual SC Programs.
NO. REV. NO.
Qualification Status List ALSEP Array A2 Configuration
ATM 986
Central Station Electronics
Antenna and Cable
Diplexer Filter
Diplexer Switch
Command Receiver
Command Decoder
Coax Cabling
90 Channel Multiplexer
Data Processor
Transmitters
Timer, RSST (Gulton)
Power Distribution Unit
Power Conditioning Unit
Wire Harness (including terminal boards) Assembly
Astronaut Switches
Flat Cable Connectors
Special HFE Terminal Board
Special Multiplexer Terminal Board
Thermal Plate Assembly
Thermal Bag Assembly
PAGE 5
OF
DATE 5 March 1971
Qualified As :
Qual SA
Qual SA
Qual SA
Qual SA
Qual SA - Address Change Qual by Similarity
Qual SA
Separate Component Qual Program
Qual SA - Data Format Change Qual by Similarity
Separate Component Qual Program
Separate Component Qual Program
Qual SA
Qual SA
Qual SA - HFE Changes Qual by Similarity to Qual SA and Qual SB Harness
Qual SA
Qual SA
Qual by Similarity to Existing Terminal Boards
Qual by Similarity to Existing Terminal Boards
Qual SA
Qual SA
NO. REV. MO.
Qualification Status List AL.SEP Array A2 Configuration
ATM Q86
SP-1 Structural/Thermal
Primary Structure
Connector Front Panel Layout
HFE Astromated Connector
PDM
Side Curtains
Curtain Cover
Rear Curtain
Rear Curtain Cover
Specular Reflector and Masks
Sunshield Assembly
Dust Detector Reel
SP-1 Experiments
PSE
LSM
SWE
DTREM
PAGE 6 OF
DATE 5 March 1971
Qualified As:
Qual SA
Qual SA
Qual by Similarity to R TG on Qual SA
Qual SA
Qual SA
Qual SA
Qual by Similarity with Qual SA with Verification from EDM
Qual by Similarity with Qual SA with Verification from EDM
Qual SA
Qual SA
Qual SA
Qual SA - Changes Qualified by Similarity
Qual SA - Changes Qualified by Similarity
Qual SA
Qual by Similarity to Qual SA
~space ···.,stems Division
SP-2
Fuel Trans. Tool
Dome Removal Tool
Unv'l Handling Tool
Qualification Status List ALSEP Array A2 Configuration
Qual SA
Qual SA
Qual SA
IU:Y, I"'U,
ATM 986
PAGE 7 OF
DATE 5 March 1971
RTG Cable Stowage Assy Qual SA
Carry Bar Upper Qual SA
Carry Bar Lower Qual SA
Boom Attach Assy Qual SA
Aiming Mech Pkg Qual SA
Subpallct As sy Qual SA
HFE Subpallet Qual SD
HFE Qual SD
Shorting Plug Qual'd by Components Similarity
Pallet Insert Assy Qual SA
Pallet Brkt Assy Qual SA
Subpackage Assy Qual SA
IPU Generator Qual SA
SIDE Qual SA
HFE SN 6 Qual D
Reflector Qual SB
Qualification Status List ALSEP Array A2 Configuration
MO.
ATM 986
PAGE 8
REV. NO.
OF
DATE 5 March 1971
1. 2 OUTSTANDING FAILURE ANALYSIS REPORTS
The below listed FRs against Flight ZA ALSEP configuration are being processed for Failure Analysis Reporting as of the date of Publication for this QSL. All previous failure analysis reports against ALSEP Qual SA, Qual SB, Qual C and Flight ZA ALSEP hardware have been closed by MSC review and approval actions.
1. FR-285, PSE Sensor S/N-3, Flight Spare
KSC DR #F-ASI-0007 reported PSE pressure below minimum value of 332 during periodic KSC pressure checks. A linear regression analysis established that the leak rate is within specification and that PSE S/N-3 was acceptable as a spare. An Interim FAR #285 was issued 11/25/70. The Interim FAR #285 recommended that the S/N-3 PSE Sensor continue to be used in support of integrated system on Arrays A2 and D as explained in Bendix Letter 70-970-3965. Following use of the sensor in support of AZ and D test programs, it will undergo modification to a later flight configuration. Follow-ing modification and test, a final FAR will be prepared.
Status:
Action:
Open
(1) Interim FAR issued on 11/25/70. {2) Final FAR by BxA Scheduled for
5 /l/71.
2. FR-All, Command Receiver S/N-8, Flight AZ Spare
BxA DR #AB8040 reported 35 KC IF bandpass shift and abnormal S/N ratio during T/V test at BxA. BxA troubleshooting per DR #AB8040 determined that the anomaly was due to a clear oily film on the inside of the receiver cover. After removal of the grease and completion of functional tests at BxA, the receiver was considered flightworthy. An Interim FAR #A 11 was issued on 12/2/70. The re-acceptance test of the S/N 8 receiver was stopped after completion of the ambient baseline portion of the acceptance test due to other test priorities.
"'"'· Qualification Status List ALSEP Array A2 Configuration
ATM 986
Status:
Action:
PAGE 9 OF
DATE 5 March 1971
Open
(l\ Interim FAR issued by BxA on 12/2/71. (2) Completion of acceptance test is scheduled
with T /V test to be completed by 5 March. (3) Completion date of BxA FAR is scheduled
for 3/10/71.
3. FR-Al5, PSESensorS/N-7, FlightA2
During A-2 System T/V testing the S/N-7 PSE failed during the lunar night IST. PSE Sensor temperature data was identical to the PSE short period seismometer data, except for a different data sampling rate. Based on troubleshooting and visual mechanical inspection, the failure was isolated to the Schjeldahl connector J35. Reference FAR 244B for a similar problem on the same PSE. FR-A15 notification to MSC was issued 12/11/70. An Interim FAR #A-15 was is sued on 1/11/71 to describe the J35 connector rework and change of connector potting to a softer material. The final FAR A 15 Revision A describes reliability analysis of the originally defective connector and inspection procedures which were developed during failure investigations.
Status:
Action:
Open
(11 Interim FAR issued by BxA 1/11/71. (2) Final FAR issued by BxA 2/12/71. (3 \ LSPO returned comments and questions
to be incorporated in later revision. (4\ Revision B FAR scheduled for 3/10/71.
4. FR-Al6, LSMS/N-7, FlightA2
During A2 System T /V test per test procedure 2345114, Subpackage I, the Lunar Surface Magnetometer LSM S/N-7 exhibited a failure. With digital filter in, all science should be saturated, was near zero and oscillating. With filter out saturation is obtained.
Status:
Action:
Open
LSPO FIAR (GFE experiment') and closeout was scheduled for 2/25/71. However, a waiver request initiated by MSC is still pending approval.
Qualification Status List ALSEP Array A2 Configuration
MO.
ATM 986
REV. MO.
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DATE 5 March 1971
5. FR-Al9, LSM S/N-7, Flight A2
During A2 IST per TP 2346320, the LSM experienced site survey anomalies and troubleshooting which led to the replacement of the 7: axis string cable.
Status:
Action:
Open
LSPO FIAR (CFE experiment) and "Technical Agreement'' closeout action expected by 3/15/71.
6. FIAR #AA-EH-OOODl, HFE S/N-3, Array D (Qual)
BxA DR #AB7496 disclosed that all probe heater current values were 0. T. during PIA prior to Array D qual. vibration test. Troubleshooting isolated the fault to test points which were exposed to shorting due to damaged conformal coating.
Status:
Action:
Open
(1) Final FIAR issued by BxA on 2/11/71. (2) LSPO closeout was scheduled for 2/25/71,
however, MSC comments and questions were issued by MSC on 2/22/71 for BxA revision of the FIAR. The Revision "A" FIAR is scheduled for completion by 3/15/71.
7. FIAR #AA-EH-OOOD2, HFE S/N-4, Array D - Flight 5
ADL TWX 9/22/70 notified that test data at ADL disclosed 0. T. failures of both probes # 1 and #2. Test troubleshooting has been conducted at ADL and it has been established that the gradient bridges shorting ratio has shifted down but has been stabilized at new values.
Status:
Action:
Open
(1) Final FIAR issued by BxA on 2/11/71. (2) LSPO closeout was scheduled 2/25/71. (3) By telecon on 2/25/71 LSPO informed
BxA that a closed FIA R is in process.
Qualification Status List ALSEP Array A2 Configuration
MO.
ATM 986
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DATE 5 March 1971
8. FIAR #AA-EH-OOOD3, HFE S/N-3 Array D (Qual)
BxA DR #AB8566 was issued as a result of PIA after Array D qual. level vibration to report the probe H 1 data output 0. T. BxA isolated the failure to the probe as a 3 O% reduction in the resistance of one bridge arm. The defective probe has been sent to the subcontractor (A. D. Little\ for evaluation testing prior to any decision on des truetive analysis.
Status:
Action:
Open
(1 \ BxA status letter issued 2/2/71. (2\ At the Array D SP #2 QAR on 2/19/71,
BxA was directed to continue the failure analysis.
(3 \ Final FIAR is to be scheduled following ADL testing to be completed 12 March 71.
9. FIAR #AA-EH-OOOD5, HFE S/N-2, Array D (Qual\
BxA DR #AB 8593 was is sued as a result of Qual D previbration PIA to report the HFE S/N-2 0/T conditions on probe #l. The anomaly was traced to a flatpack gate assembly #A72 on the P-1 00 board. The flatpack was sent to WSTF for laboratory diagnosis on 12/4/70. Further troubleshooting has indicated the flatpack replacement resulted in the failure (open' of a plated thru hole at the logic input pin of the flatpack.
Status:
Action
Open
(11 Final FIAR issued by BxA 2/11/71. (2) LSPO closeout expected 2/25/71. (3 \ LSPO informed by telecon on 2/25/71
that a closed FIAR is i:l process, however, additional information was later requested.
(4 \ Supplemental information to be provided by 3/10/71.
NO. REV. NO.
Qualification Status List ALSEP Array A2 Configuration
ATM 986
PAGE 12 OF
DATE 5 March 1971
10. FIAR #AA-EH-OOOD7, 90 Channel Multiplexer S/N-16, Array D- Flight 5
During PIA, channels 85 through 90 of the S/N-16 MUX displayed excessive leakage. Troubleshooting per DR f/AB-9403 isolated the problem to an AMI MX02D HEX MOS FET gate. The replacement displayed similar characteristics. Failure analysis at the vendor has been completed. The cause of the original failure could not be determined due to damage to the MOS gate upon rcn10val. Cause of the replacement's failure has been deter1nined to be a crack in the glass seal allowing solder flux to enter the device. Corrective action will be to change manufacturing procedure to inspect for dan1aged parts immediately before and after placement on board.
Status:
Action:
Open
(l \ TWX notification to MSC on 12 January 1971.
(2\ FIAR analysis and CAR status issued 11 February 1971.
(3) Memo 9721-2041 issued 15 February 1971 to request reliability participation on part removal MRB.
(41 Final FIA R to be issued after QA response to Reliability.
11. FIAR #AA-EH-OOODB, SP #2 Structure, Array D (Qual\
During Y -axis sine vibration, exces sive1y high g-levels were recorded on the up sweep for design limit vibration. Per DR #AB-9464, troubleshooting isolated the failure to the 2339101 pallet assembly skin to honeycomb bonding.
Status:
Action:
2. 0 HARDWARE CHANGES
Open
{1 \ TWX notification to MSC 2/12/71. {2 \ Final FIAR by BxA scheduled for
I 2 March l 9 7 1.
The following hardware changes were made to Array A2 from Flight l and Flight 2 configurations. The Applicable C RD/Justification for each change is included with the new part number:
su :KAGE I ATM 9S6 Page 13
CONFIGURATION DIFFERENCES
Flt~-i {Flt. 2) A -2
PART NAME Part Number Part Nwnber
Subpackage I
Sunshield Assy Mod.
Primary Struct.
Central Station
Thermal Plate
Harness Assy
Transmitter
Multiplexer
Timer
Dust Detector
PSE Sensor/ Shroud
2334848
2335136
2335088
2330399-2
2330351-2
2331250-2
2330527
2330524
2330626
2330370-2
2338460-ZC
Reflector Assy 2330177
Thermal Bag 2330333J
Thermal Curtain 2335582B
Thermal Curtain 2 335609B
2344986
2344990
2338947
2344957-1
2344955
2344956-1
2345250
2338900
2338511
2341440
2338460- *
Not used
2330333K
2335582F
2335609F
APPLICABLE CRD's/JUSTIFICATION
Part number change due to Configuration Differences
Thermal Mod. as result of Off-Equator Deployment
Thermal Mod. as result of Off-Equator DeploYJUent
Part Number change due to Configuration Differences
Part Number change due to New Timer
Part Nwnber change due to New Timer
Bendix Design
MOS-FET Mod
Solid State Timer Design
Modification for MSC Requireme:1ts
CRD 57822 *New dash no. to be assigned after determination o: Flight Configuration
Deleted as result of Off -Latitude Thermal Mod.
CRD 57563
CRDs 57 399, 57 455, 57607. 58928
CRDs 57401, 57456, 57608, 58929
w co
Subpackage I - (
Flt:ITFit.l) A-2 PART NAME Part Nmnber Part Number
Insulation 2335617
Insulation 2335618
Spring 2335628-
Spring 2335629-
Spring 2335630-
Shroud & Gnomon 2338016D Assy
Adapter,PSE 2338083-Socket
Terrni:1al Stud 2338174
Tab, Right angle 2338527
Handling Socket 2338211A
Diode Board Assy ---
Girdle & Lanyard 2338794C
Radiation Barrier 2338798-
Decal, PSE ---
Pad, Hook & Pile ---
Insulating strip ---
Spring Clip ---
2345636
2344959
2335628A
2335629A
2335630A
2338016J
2338083A
2338211 B
2338535-1
2338794-ZG
2338798A
2338922-9
2338924
2338925
2338926
~uration Differences
APPLICABLE CRD' s /JUSTIFICATION
Thermal Mod.
Thermal Mod
CRD 57715
CRD 57716
CRD 57717
CRDs 57469, 57500, 57595. 57627, 57857
CRD 57754
Parts deleted due to Tiiner change
Parts deleted due to Tiiner change
CRD 57723
Provodes Multiplexer Channel Protection
CRDs 57408, 58566
CRD 58635
Astronaut request
AT:T\1[ 986 I \14
Thermal Mod as result of Off -Latitud~; deployment
Thermal Mod
Thermal Mod w ..,0
PART NAME
Velcro Pad & Hook
Curtain Assy
Shroud Mod Kit, PSE
Label-Arrow, PSE
Compass Quad:, PSE
Bracket As sy
Gnomon, left hand
Gnomon, right hand
Cover, Sun Compass
Guard Assy, Left
Guard Assy, Right
Retainer, rear
Brkt. , Conn.
Subpackage I - Cm
Flt. ((:Fit. 2) A-2 Part Number Part Nwnber
2338928
2338935
2341623
2341624
2341625
2344952
2344970
2344971
2344985
2344991
2344992
2344993
2330ll7 2345132
\ . ration Differences
APPLICABLE CRD's/ JUSTIFICATION
Thermal Mod
Thermal Mod
ATM 986 ge 15
Maintain Low Backc.Face Temperature of the Aluminized Teflon Portion of Thermal Shroud
Off-Latitude Deployment
Off -Latitude Deployment
Thermal Mod
Off-Latitude Deployment
Off -Latitude Deployment
Thermal Mod
Thermal Mod
Thermal Mod
Thermal Mod
Redesigned for new Timer (P27)
~ 0
PART NAME
Handling Socket
Spacer, Conn.
Conn.
Lacing Tape
Guide Fastener
Plug, Retainer
Protective Strip
Command Receiver
Flat Pack
Subpackage I - Configurat.
Flt:·~C(Flt. 2) A-2 Part Number Part Number
2338115
2334549
095-9031-0015
50DOF17VF 721 -H
2335931-1 2335931-7
2334676
2335148
2330523- 2330523A
SL3539-4 SLl 0456
Discrete Assy, 2330855F 2330855G D/P
Thermistor Assy 2330446C
Thermistor 2331253D
Operational Amp. , 2334686G PDU
2330446D
2331253G
2334686J
Arr-986
1ifferences p ).6
APPLICABLE CRD' s/ JUSTIFICATION .~~~---------------------
Additional Part Added for Removed of New Rear Curtain Retaining Bracket (Thermal Mod}
Additional Quantity (2) added for P27 (New Timer)
Additional QUantity added for P27 (New Timer)
Old part not available
Height Changed to accommodate new Bracket-Thermal Mod
Quantity decreased by one (l) for Thermal Mod
Removed as result of Thermal Mod
CRD 57477 {Potting hole covers)
Part number changed to identify unique Bl testing of a 9041 Flat Pack
CRD 53271 (Burned-in thermistors)
CRD 53271 {Burned-in thermistors)
CRDs 5 3271, 56098, 56099
CRDs 53271, 55333 (Added Alternate Relay 2338517)
..r: .....
Subpackage I - Configure. Differences
Flt. 1 (Flt. 2) A-2 PART NAME Part Number Part Number APPLICABLE CRD's/JUSTIFICATION
Exp. Drive, PDU 2330472K
CIS Cont. Ckt. PDU 2330467N
Inverter Module 2330036B Base, PCU
Cover Assy No.1 2330039B Inverter Module
Transistor Mod. 2330040B
Cover Assy No.2 2330056B Inverter Module
C/B Regulating 2333563A Module
Transformer 2333584B
Transistor 2 3 34459-
2330472L CRD 55332 (Added alternate relay 2338517)
2330467P CRD 55331 (Added alternate relay 2338517)
2330036C CRD 53331
23300390 CRDs 53271, 53329
2330040C CRD 53326
2330056D CRDs 53271, 53330
2333S63B CRD 53271
2333584C CRD 55990
2334459A CRD 53327
A'T'-- !186 P. )7
Flat Pack SL 7275-2 U5B770931XB1 Part number changed to identify unique Bl testing of a 709 Amplifier
Thermistor GB25PM2 2335661-1 CRD 53271
Thermistor GB42MM62 2335661-2 CRD 53271
Thermistor GB42PM62 2335661-3 CRD 53271
RF Cables 2330528-4, 2334698-l ,-2 New Transmitter 5, & 6
,J>.. N
ATM 986 Subpackage I - Confi~ ion Differences p ~8 ..
Flt. f(F"'lt. 2} A-2 PART NAME Part Number Part Number APPLICABLE CRD's/ JUSTIFICATION
-~- .r:-
Wire List 2331251
Wire Diagram 2331252
Cable Diagram, 2335171 Test Config.
Battery, Timer 2334476
Multi -Format Comrrnuator, D/P
Digital Data Proc.
PSE Se~:>or
Base A:;sy,
Sensor
Heater
2330846-l
2330521 J
2341604 A
2341603 -
Sensor 2341606 Electronics P. C. Brd. Assy.
P. C. Brd.Spacer 234206-1
P.C.Brd.Spacer 234206-2
P.C.Brd.Spacer 234207
P. C. Brd. Spacer
P. C. B rd. " Z" 234540
W/L 2344956 New Harness for Timer Change
2344988 New Harness for Timer Change
z34691a New Timer & HFE Addition
Solid State Timer Used
2330846-4 CRD 58758
2330521 L CRD 58775
2341604-502 D (Heater Mod) CRDs 57662, 57709 58715
2341603-502 E (Heater Mod) CRDs 57662, 57409. 58669, 58715 & 58795
2344709-l
2341606-502 D CRDs 57662, 57696, 58669 & 58795
2344701-1
2344701-2
2344702
2344712
2 344700 *" VJ
ATM 986
Fit. l{:f._.;it-.-2>'
Subpackage I - Config .on Differences Pc '9
A-2 -----------·-------------------------~ ____ . Part Number Part Number APPLICABLE CRD's/JUSTIFICATION
P. C. Brd. "W" 2338'/86 -
P. C. Brd 234572
Capacitor, 47MF Qty. of 1 CSR13F476K2552
Transistor Qty. of 3 S2NZ10Z
Transistor Not used
Transistor Qty. of 4 2N2222A
Resistor, Z. 5K 238038
Resistor, R38 & Not used R39
Schematic, 11 W" 2338787 Brd.
Heat Sink Not used
Heat Sink Not used
Heat Sink Not used
Wiring Diagram 2341608
Wiring List
Cable Assy, SIDE
2341607
2333508A
2338786-501 A CRD 58669
2344707 CRD 58669
Qty. of 2 Heater Mod
Qty. of 4 Heater Mod
JAN TX2N3499 Heater Mod
Qty. of 2 Heater Mod
Not used Heater Mod
Select at Test Heater Mod
2344708 Heater Mod
2344713 Heater Mod
2344714 Heater Mod
4055 Heater Mod
2 341608 -501B CRD 58782, 58669
2341607 B CRD 58718, 58782
2333508 B CRD 58730
Flt. 1 (Flt:. 2) PART NAME Part Number
Connector Dust Not Used Cover (P27}
Insulating Strip 2330673
Fastener, Hook 2330330-1
RF Cable 2330670D
RF Cable 2330671E
Antenna Wire 2.334491 Cable Stowage Assy.
Pin, Ant. 2334495A Wire Cbl. Stowage
Dust Cover Not Used Mod Kit
Dust Cover, Not Used S/PI
Subpackage I - Co
A-2 Part Number
2345637
Not Used
Not Used
2330670E
2330671F
2334491J
234495B
2.339421
2339428
~uration Differences ATM986 p ~0
APPLICABLE CRD' s /JUSTIFICATION
Removes Possibility of Foreign Material Entering Connector.
Removed From Left Thermal Curtain Per CRD
Removed From Left Thermal Curtain Per CRD
58939
58940
58945
58946
CCP-2.71
CCP-271
>l \.
FACI PART NAME Part Number
Sub-Pkg. II 2334849 AC
Aiming Pkg. 2335354 E
Aiming Mechanism 2330309 -
Shorting Plug 2335520 F
Bolt. Internal 2332986 -.
Upper Hal£, Carry Bar 2335471 B
Spring, !Lock 2335474 A
Lower Half, Carry Bar 2335476 E
Post-Carry Bar Stowage 2338118 -
Universal Handling Tool 2338102 A
Handling Socket 2338390 -
Handling Socket, PSE Stool 2338117 A
Handling Socket, Aiming Mech. 2338114 -
Handling Socket, Rtg. cable 2338116-
) '--~·-
Su.wr'ACKAGE II
CONFIGURATION DIFFERENCES ATM 986 Page 21·
A-2 Part Number
2339080 B
2335354-1 F
2338987
2.338017
2332986 A
2335471 c
2340985 A
2335476 F
2.338118 A
2338102 B
2338390 A
2338117 B
2.338114 A
2.338116 A
CCP/MSC Auth.
262
245
245
250 250 A
050012
OS0012
245
245
2.45
245
245
245
APPLICABLE CRD's/ JUSTIFICATION
Redesign For HFE
57928
Addition of 180° Slot (Ref. CRD 57928)
Central Station Harness Assy. provides Mu: Channel Protection
56244 Used on Flt. 4 and Flt. 3
57700
Provide more positive locking CRD 57700 & 57796
57704
57759
57763
57756
57753
57757
57755
...... -·-·· r-- ------------
Subpackage II · .1£iguration Differences ATM 9~6 ··Page 22
FACI PART NAME Part Number
Adapter, EHT Socket 2338119 -
SIDE 2338104
Housing Assy, Shorting Plug 2335598
Housing, Shorting Plug 2335627
SIDE ICD (Mechanical) 2323521 J
Pallet Assy. 2334901 M
Lanyard, Shorting Plug -Ammeter, Shorting Plug 3204-367
Pedestal Assy, SIDE 2335362 B
PSE Stool 2335945
Lanyard, SIDE, Boyd Bolt Not used
ALSD ICD 2332263
Cable Assy, SIDE 2333507 c
Riser PSE Stool 2335945 A
Dust Cover -Dust Cover -
A-2 Part Number
2338119 A
2338104
2338008
2338020
232352.1 K
2339081
2339198
2339470
2335362 c
2344723-501
2339487
2332263 F
2333507 D
2344728 A
2339468 D
2339449 A
CCP/MSC Auth.
245
229
262
250
250
255
272
265
271
271
APPLICABLE CRD' s / JUSTIFICATION
57764
Change source nan1e from Marshall Labs to time zero
Different Shorting Plug used (Mux. Channel Protection)
Different Shorting plug used (Mu.x. Channel Protection}
57804
Modified For HFE
Added per CRD 58632 to 2338017 (C)
58773
58708
CCP-265
58854
58732 MSC LTR EH2 L193/B201
Redesign of Stool
.... ~
Cask Dome Removal
Tool
Pin Lever
Pallet Insert
HFE Sub Pallet
Astromate Conn.
Subpackage II - Configuration Differences
FACI A-2 CCP/MSC
.L-u:M 986 Page 23
Number Part Number Auth. APPLICABLE CRD' s / JUSTIFICATION Part 1\
2337954 D 2337954 E 58936
2338125 A 58937
- 2339081 262 HFE Add it ion
.. 2339130-101 262 HFE Add it ion
... 2339160 c 262 HFE Add it ion
··c: ~ --..
Qualification Status List ALSEP Array A2 Configuration
.......
ATM-986
PAGE 24 OF
DATE 5 March 1971
3. 0 QUAL TEST HISTORY
3. 1 SUBPACKAGE #1 ASSEMBLY
With exception to those areas discussed below, Subpackage 1 was successfully qualified under the Qual SA Program. The QSL sheets provided in Appendix B for Subpackage 1 reflect the Qual SA test results except where noted on the applicable sheets or discussed herein.
3. 1. 1 BxA transmitters, P/N 2345250, S/N 26 and S/N 27 (on A2) were qualified under the Qualification Test Program performed on the A-2 Qualification Unit Transmitter, P/N 2344600, S/N 23 and S/N 21. ATR 266 details the history of the A-2 Transmitter Qualification Test Program. The details of the qualification testing are itemized in the Appendix QSL Sheet B-8.
3. 1. 2 Dual 90 Channel Multiplexers and 8 Bit A/D Converters, Model 2338900, S/N 11, were qualified under the Qualification Test Program performed on S/N 7 unit. ATR -236 details the history of the Qualification Program conducted for S/N 7. The details of qualification testing are itemized in the Appendix QSL Sheet B-9.
3. L 3 Resettable Solid State Timer (RSST), S/N 005, was qualified under the Qualification Test Program performed for RSST S/N 002. The duly apprmn~d qualification test procedure covering this test is 13877-992. The details of the qualification testing are itemized in the Appendix QSL Sheet B-12.
3. 2 SUBPACKAGE #2 ASSEMBLY
The qualification of Subpackage #2 was initially accomplished as a result of Qual SA system level tests which are itemized in Appendix B, QSL sheets provided in Appendix B for Subpackage #2. The major change in Subpack #2 for A -2 is the inclusion of the HFE and the SP #2 qual is as stated below.
3. 2. 1 Heat Flow Experiment (HFE). The HFE was originally environ-mentally and functionally qualified as a result of system level testing on the Qual SB Subpackage # 1 configuration. The requalification for Array A -2 Flight Unit S/N 06 was accomplished on the Array D SP #2 Qualification Program. HFE S/N 2 was used to qualify HFE in this qualification program. Figure 1 shows the status, sequence and configuration of the Array D SP #2 Qualification Program. The system level parameters for this qualification are listed in Appendix B, QSL Sheet B-24, are those which are identified
in the test procedure of Figure I and BxA document TM 598~ Revision 3.
Tt·::.t Co::iig ..... r<ition
Z333~tJO-~ S·~b?ac~a.ge
Ir.cl"rl:r:g: HFE S/';'; 3 AL5D 5/N 3
F.Z Assy
Qi.:AL!}·;r· J , ~ '" ·-r·· _):\ :. \ ")1 ':-, PH.\5 i
d:rt.J1et~·ci ..... --
lr~F~:-_- PL·\ I' j'::;~ )PT\ '::)/;..:.. 5 tPo""t ::.::~ !
L~ _____ _ _ 1 I •.·i,·on) C./':'-1 3 !
~_:_333o6~j . tT.? 2335Jo'i1l ~ . ---,-_-
E ,l~b~e~y-~d~ir;g
1'. '6 S t
19-
0! icpnz ~/''. · cp,;2 c;~•l' IVihrdtion .: .. J Pro~s SP#Z- S/Nl6 1\'c•d:·,ca:i•m I!! p)\~ ~·~-et·;.,.
1
loTRR I fMASS PROPSl~cc-;:pt-:- v~·b'_ f[;;,~Li·;,-;~ '"';\!agneticd-r~"hock___ jl'l;~(l Bo:t- --l · '0--a, p-=:-~~ · : ____ ___ _ _ .~__ . ·'·' 1 -----~ - · ~- · ·' ·''r, 1 97G3-359 • ep. I -~-· - ~ ·' 1b ~ " - ~ ,, 0 rpf2 "'N'li> SP 2 S/".16 . <;p,? SI'"L, ' ~. ',, •. . _l . _J TP 233?J2n I TPZ3-±70b2. [TP 2346.!2.81 TP 2333049 j iTP 2346329 ~-~--p-gE:~ \ 128 Oct. 1979
~llOJlr.g ~!ech. Funct. SIN 4
· -i'-:PZTI~
----- O'CALIF:CA -f-ION EVENTS, PHAS:-:: II
:2.·=.~~_::-~~Test Configuration
.!3339:J;).2 S<lbpackage #2 Ascy
.Lnc-lucii:-,~:
D\.7-EFS W/0 Astromate Conn.
:-;o·i-E: ALSD has bee:: deleted from Array D
~rTIOO:.ficahons I I Ito 5? ii2 I ' f---------. j L_ __ l_j I Stow SP #2 I W/DVT-HFE
,L_ i !
F>re:c:);;-a:I;
;,;:;;:·::" d l (HFE ::-pr:;,._--,' I I S/NZ ~ p5rruar =:j
Events Completed
_______ ...__ _______ ----------- ------.---:---:::~:-:---::---:
[
--________ q_1,0~l::I_c::~·~l(?~-~VEN~_PHA5'0.!I --------·---~- :h?ack~ge .,z Test Confi~t:<ration
233>?1:!0-2 '>1bpackage 112 Assy
bch:d:~.g: HFE - S/N 2
:\OTE: AL5D has been deleted frc.m Array D
R etes1 Events Con1pleted ... \1agne,lC Preas n I'eot Comp. l'O.:t. 1 70
I, -·all HFE- I f !iF•, · PIAJ' 1 ..... ~~ .... LP,Jsr-tS/N 2 on I ~.r.\':r0n) _j ISP "'2 I 5 "'2 ' ~ TP-z?-33069 !
fMOSs~ro;>$1l Acc<'pt. ~ib. r~s-_. l,indt Shock I~O\';:r:: II I QAR ~ SP ff2 - SP i/2 • nbr.l~ton SP 1;2 - \<>clhcat,:q'l. S/X ill6 S/~ 16 _J 5P~~ - S!Nl6 S/N 16 5P~2 -5/N !6 118-19 Feb 197 ~~3i93'.Ji ~~ ~ ·~ . ~ f-,..,=;-,---cc7·;- n ~~ ~ ' 'n ~~' '~M
DR <i4o4 Repair P;ti1et DR 9• l3 Replac: Esna Nuts (I'oydoolt)
Figure 1 - , P fl A v D SP #2 Q:'/ • :FICA7<0N PP CCi,,. 'v! STAT U.S.' 5EQ'C'ENCE/CONFICURA TTON
)..~ TJ.v~ 9~;6
Page 25
TP
IST-2333034C Replay- 2333034D
2333060A
2333087
2337925
2337938
2337939
2337940
233794I & 2337941A
2333034D
2333049
2333049
2338178
2334335 -Environ. 2333032B-IST
2334346-Design Limit Baseline IST
2338600-Modified IST Vib. & Mod.
Qualification Status List ALSEP Array A2 Configuration
NO.
ATM 986
REV. NO.
Section 4. 0 QUAL TESrr ~"~l':PO'"<T
LIST
PAGE 26 OF
ATR
48
4I
33
43
42
69
30
40
49
68
79
39
70
97
83
DATE 5 March I971
SUBJECT
Baseline Integ rated System Test
System Crosstalk
System EMI
Central Station Power Dissipation
Mass Properties, SP #I
Mass Properties, SP #2
Acceptance Vibration, SP #I
Acceptance Vibration, SP #2
Post Vibration Integrated System Test
Magnetic Properties Subpackage #I (Stowed)
Magnetic Properties Subpackage #2 (Stowed)
Stray Field Magnetic Properties (Deployed)
Thermal/Vacuum Acceptance
Design Limit Vibration SP #I
2334348-Design Limit 23330I5-SIDE Modified PIA 85 Design Limit Vibration Subpackage #2
I r.u. tn:v. rev.
Qualification Status List ALSEP Array A2 Configuration
ATM 986
PAGE 27 OF _Z_7 __
TP
2334328-Shock 2338600-Mod. IST
2334331-Shock 2333015 -Post Test Veri
fication SIDE -PIA 2333057 -(page 7 only) RTG
Resistance
2334343 -Acceleration 2338600-Modified IST
233433 0-Accele ration 2333015-SIDE PIA 2333059- RTG Functional
2334345-System Test 233861 0-Environment
233 8617 -IST 2338610-(Sec. 6.9)
Environment
ATR
87
89
91
93
102
104
266
236
DATE 5 March 1971
SUBJECT
Qualification Shock Test Subpackage #1
Subpackage No. 2 Shock
Subpackage #1 Acceleration Qualification
Subpackage #2 Acceleration Q ualifi cation
Mission Simulation
Design Limit Thermal Vacuum Test
Transmitter
9 0 Channel MUX
Qualification Status List ALSEP Array A2 Configuration Appendix A
NO.
ATM 986
PAGE AI
REV. NO.
OF A7
DATE 5 March 1971
APPENDIX A
QSL SHEET COMPARISON CRlTEHIA
The qualification status defined in the Appendix B QSL Sheets {BxA format 970-12) is presented in a manner to compare ALSEP equipment specified environment or parametric requirements to the stress levels achieved during Qual SA or previous programs.
The qualification status has been established by the qualification testing accomplished at BxA and is reflected on the applicable QSL sheets by the listing of the appropriate test procedure, test reports and remarks relative to each test or to prior qualification tests.
Qualification testing of ALSEP for vibration shock, and acceleration was required at the system level only. That is, all equipments that comprise ALSEP were subjected to design limit levels for a stowed configuration, simulating the mounting of ALSEP into the LM compartment. The qualification vibration levels are depicted in Figures 1 through 5. These levels are in accordance with those specified by NASA Letter TD3/ L023/ 68/B- 26 (JAC ).
The qualification testing of Qual SA required testing to qualify the Array SA sunshield and astronaut switches. For the induced environments test, a Subpackage #1 was employed with mass simulators used for the previously qualified experiments"
The qualification levels for the Trans1nitter, RSST and Multiplexer at the component levels are as indicated on each applicable item QSL sheet in Appendix B.
The SP#2 and HFE requalification was accomplished per BxA TM-598, Rev. Band the TP 1 s listed in Figure I, in Section 3. 0. The qualification vibration levels for Array D SP#Z are the same as the above Figures for Qual SA with the following exception. Figure 6 shows the Earth Launch Boost Vibration I_,cvcl for the X Axis perforrned to Qualify SP/!2, Array D.
··wa1~,t~aoe . ~DhllaiM
10.-0
..0.:: fl$ Q,)
0.. 11119 1.5 I
c 0 .... ... nl Po< fJ -tl u· 0
< .... 5. I:: -
5
,, ~! .. ';?!!;
!;,, '·7f'~~:~: . ,._"'
'I
Qualification Status List Appendix A
NO.
ATM 986
. PAM A2
UV. NO.
MTI 5 March 71
•
---!
I I
' I r
' ' I I '
lZ
•
"' '
Sweep· R6t'C'J : 3/4 ·Octave I Minute ($ .. lOp .. 5 ~). g ... peak · Tolera.nce +10%
, , I
Frequency - Hz
Figure 1
·I
I f
t I I 0
,
..
Ai811011p 8100 . ...-~ Dhfitllon
Qualification Status List Appendix A
A3 PAGI 011'
DATI 5 March 71
Test duration 2. 5 minutes power spectral denBity tolerance I} db
,
(JJ
0. u -..!.----------N 0.0 I
10
,
I I J
9 db/ octave
200 400 600 1300 2000
' . . •Frequency .... Hz ·.,
, Subpackage 1 . Earth Lat.tp.ch Boost. Phase Random Vibration Sp,ectrum besign Limit. x ... A:d$ only
...
'fl a.· u -N 00 I
.... ..... en c
. 1
Qualification ,Status List Appendix A
1140. I IIV. wo.
ATM 9861
PAGII A'i
OF
DATI! 5 March 71
Test Duration 2. 5 Minutes Po wet Spectra¥1 Density t.oleranc e +3 db
~ . 01 - - - - - - - -- - ---I Q
•
I I I I I I I I
I l
Frequency -Hz
Subpackage 1 & Z Earth Launctt·Boost Phase Random Vibration Spectrum Design Limit,-' Y -Axis only
Figure 3
9 db/ octave
I I I I I I
' I
00
~ace ·~~
Qualification Status List Appendix A
ATM 986
F'AGII! A5
DATI 5 March 71
1 Power Spectral Density Tolerance~_3 db Test duration 2. 5 min~tes
9 db/ octave
c:l) • 01 - - ._ - - - - - - -- - - ,..--------...1 ~ I (j
~ ,. tl()
•
c:l)
c: Q)
Q ..-< rd ,...
..... ~ . 001 0.
(f)
,... Q)
~ 0
11.
Frequency 1-Hz
Subpa~kagt~ 1 & Z
I
'
I
' I
I I
80~ l 00 1000 2000
Earth Launch-Boast Phast Rand9ftl Vibration Spectrum Leve:l. Z·Axis only
Figure 4
,.
..
_/A .. ~
~~
. 1
. 01
ID 0. (.) --N WI I
>. ... .... Ill s:: ~
0 -Ill '"' .... ... (.) Q)
0. (/)
'"' Q)
~ 0 ~
. 000\
Qualification Status List Appendix A
ReV. MO.
ATM 986
PAGE A6 OF A6
DATE 5 March 71
Test Durat~n 12'; 5 nnnute" Power Spectral'Denafty t-3 db
12 db/ octave
------ ,-I I
1 I I I I 1 I I I I I t
I I I I ' J I I I I I
I I I I t
I I I I . t
' I
' 10 .. 20 l 100·. ;llt1 2000 #
Frequency -Hz
. . Subpa~fi 4 &t Z . < -Lunar Def!Jcent Random lSi'~loft Spectrum
~ign tdimit. .AU Axe~-f ·
F.igure 5'
::"'-.
"' t:T, ,.:.:-.
N
te I ?.
+> •..-!
(J)
r:; ~)
Q
Qualification Status List A LSEP Array A2 Configuration Appendix A
NO.
ATM 986
A7 PAGE-
I REV. NO.
A7 OF
DATE 5 March 1971
NOTE:: IgnOl'<' possible indicated out-of•tolcrance condition~,; caused by X- Y plotter bg below 100Hz.
I~~~~~ _ _: __ ~p_.:~:~~r<:..lJ?~~:_::i!:Y __ :I~~~~:_:~~~-::_: :Uclo; except that at a.ny ;~ivcn tinw during ihc test run a rnaxhnum of three (S) channels arc allowed a -l 6~ -3dB tolerance (all other channels
within ±3 dB}. grrns to] crz•.ncc: . :1:10% grms Level: 6. 4g ±_ 10% =64. 0 (.+ 6. 4) mV Test Duration: z.. 5 1ninutcs
.\ 3 - -- - - - - - -- -- - -
21 d 6/ oc:n;vt.[
1
I I I I 1 21 J 8 OC..TI1Vlt
I I I
C ·~ ) \ -· -- - -· . -- I l
-~-~~~ kB/oww/2' .o z ·-· -- ·-- ·-· ,_ ! I I I I
. 01
• CD\
I I I I I
I l I I
I
l
I
I l
.I
I
I I I I I I
I 280 1 600 I 1 1 (~e F) 1 (O;:t~) I
_________ . __ _j _ _j_j _ _j_ __ !_j__ ____ .
I 0 ISS £30 4-00 1300 eCOO
200 I
Frequ.ency-Hz
f~a.rth l_;;:n{nch·Boost!Phasc J.'t;tndorn Yjbration .1:_)pcctrum De sign Limit Oualifica tion Level. X 1Axi-?··
Figure 6
QUALIFICATION STATUS LIST -ALSEP PROGRAM- AS~F:I-tBLY, su BPACKAC;E #I lDate 3 iS ;71 ~~o. A T\l-" Oi, jRev. No.
!Analyst l Page of Pages
Env i ronn1ent Stress Level Verification of Stress Level Capability
Item and/or Document Remarks l'\omenclature Parameter Requirement Capability Agent Location Reference Date '(
See Note I.
5'-'~>?at. :-.age •1 E"VIROc:\IENTAL
ExA 23->4986, Tt.:r:-:ort..'rat·1re: TP2334335 Successfully Qualified
S/N 16, Ope :rating -300°F to +250°F -300°F to +250°} Bx.<\ Ann Arbor, Micr TP2333032 6/IO/bB on QSA
F1ight 2-A !\on-Operating -65°F to +160°F F:xt<'rnal SP #I ATR-60, 70 Earth ·300°F to +Zo0°F Cc;nditions BSR-2367, 237& Qualified on Qa M0cn
SA Qual Pr'' ~ ~~~1 rt! 2334&48, S/!'<3 Operating
-12 BxA Same Same as above 6/I0/68 Test level limited by lest
10 Torr Tested to ' 1\onpOperati~g __ SL to J0-12. Torr 5 x 10-6 Torr equipment capabilities
Humidity Designed to meet Operating N/A BxA Same N/A N/A NIA
1\on-Ooerating IS- JOO'", Requiren1ents -Vibration
Operating ,:; I A 1 Testt'd to Design TP2334343
Successfully Qualified on See appendix A Limit V:b levels ATR-82, 83
?'on-O?erating BxA Same 6/28/68 Qual SA herein. indica ted in DSR -2402, 2403
Launch 1.: Flight Figures l-5
Lunar Landing -Acceleration Tested to H. Sg TP2<34H3
Operating NIA I 111in~:te (hrat.icn B"A Same ATR _q(l, 91 7/4;(8 ··.ctr.J(' as above
t~un-Operating 14g-axis (',1Ch axi~. ''·SR-Z4l2, l413 Si: ,,.-,k_ 1 (•sted tn 1 S± Il-)l33432ts
c :>·-~ !"?: ~ ~!lt! ~/A ~!' II m5 saw- PYA Sa rr1c ATR-8t•, 87 b/2l.1 / t•B _...;_:unc as above
~>,n~OtJ~rating 1 ':c- I I ms · •'•!h f';;J.C"h axis l\S R- 240 h, 240/ Salt Spray :;: • .>, \ :~o 1 e.5t Rc:o·Jir('d Sar.d i: Dust ~-:.,t rfcfh.1•ri ~-o :est Rl'G .:rL"d F .;ng-"s' " .~ :~.) Te~t R(.'aJii't.'d Acvustical !'\oise :~ •t <!efi~-:cd -::o Test Reg,·Jtr-ed Rain :\'A :\o Te~uired Radiation LED-S20 130W lftt B> >\ ,\:-~n Arbor ~1ic 1 1 TP 2337912 6/10 't->R ~rr Ot'~ .. rotir.£, T('r1t:""'("rature ExC>lC1~i.~Jn Proof :..;; A ,,. ~~ ... • R~·c .. rerl
PARAMETRI!;; Tested as part Capetble of start-
Functional nf the integrated up and operation
6/!0/68 Qualified on QSA s.y~tem in space lunar surface TP2334345
Performance "in1·11ation
BxA Ann Arbor, t-.tich TP2338610 8/7/68
ALSEP TM--:;2 , ~1.· rnUer ATR, 101-102 --
G"11\ ,.,
Sheet...1,U_ of _zs __
I
·. 1 • .., :::. -; •, \ r \1 · , · '' \ · .-...
_:~_ned) !:>l R O. ,I. Fa~~· __ ,lf --- i- .1~_• QUALIFICATION STATUS LIST·AlSEP PROGRAM 1·1'.\t. K.\( ,L I, A>~ fL:'~:';:\ :\SSL~-11\LY
Rl·\·i=--~·d I :, l 11'< 1 r ~~- .
I I I t Vcriflc-atlon of Stress Lt..!vt·l Capability 1
!::nv1 ronnv:nt
and/or
ParanH:ttr
Stress Ll'\'el
lt(.;[l,
l'·~)lT\t:nclatu re
Ar.:• "·" A-.,, rr :,1-,·
a: _.. ·:·t !"':::a
Dxr\ 23?u307,
s :-: 1 1, FlL''t 2-ll ~A Q~al 5 =" 4
• d ~) ~ ('
B ·:A 2314522,
s " 11, ?light 2 -A
":\ Q·aal
2 "030), s :-: 4
\ .... ~. -: '"'R ·~1n1 \a 1 r>,_..:; ~- ~ :·
--::7 ~ 3
-.:_-\ ~333354-l, ' ;; f:, :- li~ht 2-A
·:.\ Q·:al
233535-t s :--: 3
'lV-12
r.:\ \' IP o~:~.! E:\TA L Tt.:Il1tJt..>raturt::
Operating !':vn-Operating
Earth }..!Jon
PrtssL:rt"
C•peratmg :'\un-Operating
HcHnidity Operating :-\un-Opcrating
Ytbrat1on
Operating
Requircrncnt Capability
Tc.stt•d in SpJ.t.:e
o c I Siin'..d~ttic•n - 25° F to+ 300 !· Ch~mber for
o o temp t•xcursions -65 F to+ 160 F of_-. lOQOF to C\1:\ +'"O"F
-I 2 J:-,10 mm:k~ S>;:~i. L to 10-· mmH··
\"crif1ed to Sxlo-b T,_)rrs 1n
Sp~cc Sin1 Ch;"ln1
Ag<'nt
BL'ndlx Aerospace Systems
BC'ndix Aerospace
Systems
o,.,,,:ncd to nwc, nendix Ae.rospace ::-:.;A IHumid1ty Ht•q'mt Systems 15'". tu IOO<:c H!l
Te~ted in stowedl BendL"'< Aerospace :--;I A I confh.:.uratic•n to Systen1s
!\on-Opt: rating H··fcr to ATR-lf \·ibr"ltH)n desi~n
Launch & Flight \{:dcndum 1 lll:1lt~ Indtc\tcrf
Lunar Lar.ding 1n F1c~ 1 thru t;
Location DoLun1ent
Reference
Ann Arbor, Mic·li1P 23Hll5
ATR-(0. 70 I\S R -? 3 1:1, Z 3 7 b
Ann Arbor, Michl T 1'2334335 ATR-(•0, 70 BSR-Z3.Q~
Ann Arbor, l\fi.:h !'-:/A
Ann Arbor, ~:;chiT. P. 23HH6
ATR-f2. 83 !}S[\ -2402, 2403
Accclt:ratiun Tf·S!t~d ir: :->tO'\Pt1
r \.'!' H:-.. Acrospil.CC Ann Arbor. ?\:ic-1~ fP 231 n-~' Opei"ating ::.!:\ ~ctt~j'1~~;,!c~n 1-l ·:·s:f'ms .-\TF .. -')~~. r..lJ
~on-Operating :\TR-16, i'H!d. 1 ~ .... ~~ ,. :1. 15 ...... !\ -2 ~12. 2·tl3 sr.r_,('k I e~tt·d Hi ··tO.'."t ,; :~cndix Af'rospa\..'C Ann .~\rbor, rdll-i {p .~ ~ \..f L~8
._(>r;fc~ Ir,•tH 1 l1 S rstC'n\S Operating :\';)n-Opt!rati!l:g
~~~trj s;r~~
c:; .-\ .\TR-11>, _.\,ho.
,\
~ 1")_ =:.2t'
I ,:..u,ustical 'i\oise ;.;_}_.\
Rd.in 1:-..:.\
l>;~±~:,llnlS 1 l.\ tin"lt'~ <'.t ;,,.;..,.
A.TF.-::-.~~. ?.i 2-!'"'t-. Z~()(
E>,Ct'Ld!' Ht.•C B··~d J .... , -.r,·~·~:, '-'··lltbf:dd. lc!:ch Dv1"11.:n \" ... ·nf.
Date
~!.ty- June
1%8
'!\/A
June -July
1968
July 10'-S
.. T._J\•
!O,S
_r .d' t: 1 "'t~ 7
Reu:.arks
Qt:aliii(:atl~''l ~'f the An!·"~'la ·\~s\· ba.<=. lJ,.l,, ;t, ~o.CJ1~l~;! ... h,·r~
at svstem levt"l d·,Hirq,! Qual SA.
-·:·-· ~~ ... ,: J.:- ·.-.~ b·.· t·:-st eq..::. ::-:::e~ ~ -:.:-3· ~:.~ ·: ~ • ~ "! ~
In stowe': ..:o:~::...:~:rctio:<. tl·t> airr:ing n1ech ·1:isni is n~o·.! ·f>~: on~- P=2. F~-fer to AT\t-77, for' -A'.i.~ 1' ·· :.,'i" \ i'·r.1t\,•·.-.
-· .. : .. llf''.t: ':-rtlo L·. "" 1: ~('('~t F!·,::t:;;('
i \ \. : . : ~. .·\ . .., . ~ F"::c.:s~3~:;~:.\~g~ ~~~~~~~~~~~~-!
~adiati.''~ I.FD-;~0 Fx\. t·t·ds: Re' Bt•ndix Rt~search L<lb~ ~-'Uthfit~ld, ~1iLh ( Dv~q;n Verif. I J>J.ne 1967 ! Vt_:::·:e~; A:-. .,:·. ':'iS I ..::.:J::losic·n Proo~ ~..: _1 A
l'AH;,;.!ETR!C
E- :~-!~·--:Power
(E:f. Bt>?...r:l\\idth
T -a:-.smlt/ Re~ei·:c)
lnp'lt YSWR @Trc,r.smitter f 0 •
@Rece1·:er £0
~~!::1nnum Puwer
-12. 5 dbm 2.7°(c, II. 7 db 270\Q 11. 0 db
]. 25: l 1. 5: I
1. Sw CW
-12. 5 dhm 290@. 11. 7 db 31°@1).0 db
1. 25: I L 50:1
I. Sw CW
Bend1x ReseZtrch L'b•l Southfield, Mich De.sicll Veri£. R<'port ~40l8
Bendix Research Labs( Southfield, Mich.( Design Verif. Report #4028
1-hndlino Capab:lit\' I @Tr,nsmJtter f 1 @Transmitter f I Bendix Research LabsJ Southfield, Mich J Design Yerif. 0 0
~.1-~xanum Aiming Error
I. Jl, 0 RMS 0. 75° RMS Design Venf.
Report #4037
Jlffie 1967
Fe::.t t::1\·i ro·'.r:':'""' ·.tal f•.;:'.l·~ic-':a: t\·;:;·~ :''.!Ce-::-:'..:1~-.;
pyr!orn:t.·d o~. t:,e an:\~n"la at-scn1bly at Hx I\Psrar(·h
on a 12 ~--..per Tt-1 2\; ...... z·l and C.oct:.mt···t('r: lJy RPport B?.L=-1•20
Sheet~ of ---
QUAliFICATION STATUS liST-AlSEP PROGRAM O:~TRAL S'~ATIOX J.:LI-:C i JW:,ICS co:-t I'0:->1::-> rs
j'>ate3571 F··AT\!-'·,,·p~.-•.
1.\n;tly:.t R.l.ntt'l 1 f'af,'-' ___ ,f ___ Fa!..'·
Item !'omenclature
F::ter, D1plexr-r
b,.\ · Z33U52.5
::;; "\ ot F'li~ht 2-A
')A (Jual, :..,, . •
970-12
Environment and/or
Paramt<ter
£X\' IRO;o.;!\!E"'TAL Ten)perature:
Operating ]\;em-Operating
Earth 1\L,on
Pressure Operating
f-_.:"'·•n_- Operating H'-lmldlly
Stress Level
RequircnH:nt
-25L\F to tlc0°F
-t>5°F to t I t•0°F
<'..10-12 Torr ~ n t 1 1 . ~ T ,, r r
Capability
OK per req1n
OK per reqm
1 x !o·5 Torr UK
Operating IOOo/o Rli at 1600 ]\;on-Ooeratin 5 t -. I 0D"c R. !! I OO')o RH at 120°!
Agent
Rantec
Wyle Labs
Wyl•e Labs
VeJ·if1c~1ti~m of Stres~ Le,·~.·l Capability
Location
~labasas, Calif
I Segundo, Calif
·.!Segundo, Calif
Document Reference
Rantec
#o6279-QTP
Date
2/19/67 2/6/67
2/20/67
2/8/67
Reli1arks
I. Qualitll-t':'·~-. \·er~i·J,•d
in SP*='l Q.;~i S_'l.. tt?-FOt
I ·r (Qua1ifi('d in s\·st{·n; tr'
::- ··: ! t + • r r v)
XA
v.·)ratir_)n-l);..··r -·.:· ~-' 'l. -----
:-.:-.Jr.-Opt:rrt.t::.L~
Acct..> h. raticn
!\un -O?erati~g Shock
Operating ]\;on-OperatinE_
Salt Spray
R-o;.loon: IS t'2 '50 cp;, 0. 2g ''-jPUK p<'r reqm . ...::tn··:S t,"> 20 cp::; ,l 4 :n. n . ..\. 20
"~1.1 cps vg
>~ .\ OK per reqm ..:: ; :: s (.'>,""!. <t" \..;
'.;: . .\ 10!-: po•r re<;;n, ~n t:'s ea. ;,xl~
:-; ·' l'<t.-\
2/ )3/67
2/10/67
' 2/9/67
Sand & Dust '.; .> '.-\ T T l T T
See rE'n~o rk l
See rPr~~ark
St:>e rer-:a rk
I F "'g'' s .\ '"' I T I I _j - ·-1 .'.coustical ]\;oise '; .-\. ; .~ I I 1 I -~--- --1
Ram :;,.\ :.-\ --1 Radiatir.~n :F.~.1J
Explosion Proof PARA!-.IETR!C
vs.·:R
Insertion Loss
Isolation betv.een Ch~nnds
? ~'it lt•.·ri ~t fo::-c. i;?.db
:' .. ·\ l'o: I A
1.3b:l !-.l-1xall ports
0. 8 db Max
50 db f r to fLO
KO db ft to fr
I. 22:1 max 33 ~1c 1-!i.l
0. 73 db max
90 db min 7 100 db min
-B-unKe·rtla mo
Rantec
Rantec
Ran tee
""~n,1_~1 P:~ rk Ccd! ·1 ob..':i"Q-QTP
Calabasas, C•llf.
Calabasas, Calif.
Calabasas. .Calif.
66279-PTP-D
66279-PTP-D
66279-PTP-D
2.,. .!..2 i t•7
Before and
?.fter each l : environment~ I test
1/16/67 to 2/23/67
1/16/67 to 2/23167
IJ
Q•.:.alif1er! as pa· t nf a1
i!·.tec.··a'Pd S\'Stf"~"': 1•· .;.t•
spa ... t" si:!1.'dat\t'::, i'.u~· ... r d·_tnn.: Q.:al 5 A
TP 2333032
PTF-iO. 70 .r·:!1E> l Q, ..(
Sheet_li.L_ of ---
. ..
QUAlifiCATION STATUS LIST ·ALSEP PROGRAM C I '; T H A! S T •\ I i 0' F I F C. ! ; ~ I- • II
COl\! PO;.;~:~; rs
En;. 1 ronn1ent and/or
Paran1eter
Stress Ll'vel Vl·rift1:ati'-m of Stress Level Capabdity
Itt-n1
~;:.~menclature
D~pi t·xer ..... ,i BxA ·~330526, ~ ;.: 9, Fli~ht ~-A
SA Qual, S ':-< 5
97J.l2
E~: "liP u;-:~.! E:": TAL I en ?erature:
Opt• rating !\on-Operating
Earth l\1 .. 1l)n
Fressurc;! Operating Non-Operating
Humidity Operating '!'\ un ~Operating
V1~rattl1 n -:..'r~,r-it·
l'cn:·Operating
R equiren1ent Capability
-Z5°F to -!boo;.-( OK per reqm.
-oS°F to -1 o0°F I OK per reqm.
10-lZTorr 30 tu I. 3 Torr
!3 tu lOO""o R. H. '\I.\
1 x 10- 5 Torr OK
lOO'"o RH at !&On 1007, RH at 120''
~~ :tnJ.l"'n1: IS to2 l :;o c-ps, 0. 2g I 1Ps OK per reqn1
'-.,lnt:; 5 to 2.0 c.p~ C'. ~ "'- D .. -\. ~0 tP lOO cps, 8'~~
Agent Location
Rantec aiabasas, Calif
Wyle Labs 1£1 Segundo Calif
Wyle Labs f:l Segundo Calif
Acct·leration
Operating XGn-Operating
Si--.ock
~/A . ' ~ 23~'s e" ""15 I J,
OK per reqm.
Operating ;.;tA OK pt:'r reqm ;-\on- Operating 20 ~':-; ea 2Xh
S;;.lt Spray :\ .-\ ;.;j.-\
s..~nci t.: D•1st .-\ :.:. . A F .f'\:;'1'5 ·;,tA "-' .-\ Aro•1stical !'\oise ::I \ ;.;.'A Ra1n :.; I.-\ ;.; ! ·" Radiation R :'ld1~ted <'!t fo:~ t 50 db Explosion Proof :.:,; .-\ I:--:; A
PARAMETRIC vsv; R 1.36:1\!~x fl.2l:lmax
Insertion Loss 0. 7 db !t!ax
Isolation between 120 db ~1m Port Channels !\ to Pori B or
vice ver..;.a
** 2119 rnc and 2277 me
( 130 !tic min)
0. 63 db max
22 db min
\
Bunker Ramo C>noga Perk Cal·
Rantec alabasas, Calif
Rantec alabasas, Calif
Rantec alabasas, Calif
Docurnent Reference
66279-QTP
66279-QTP
....
66Z79:_QTP
66279-PTP-S
66279-PTP-S
66279-PTP-S
I •:.'. • ; - 1 ~- ·\ ; " ' I . '· . :\llalyttt R:tntt•t I Pa~t.' ___ Ld ___ .i-·.1:.:_\ :-.
Date
2/19/67 2/6/67
2/20/67
2/8/67
2/13/67
2/l0/o7
2/9,67
2/22/67
Before and after e!3ch environmenta test
1/16/67 to 2/23/67
I/ 16/67 to
2/23/67
Remarks
l. Q\lilhit,·~1\,·n '"·eriilerl in
SP= 1 Q~1a! 5A t(;> st.
Qualified in S\·stem to 5 x 10-f- Tr,rrs
See rerr:a rk l
::-:ee rt::':.:a rk
See re!~-:ar~ 1
: Qua lifierl as part of a ~1 \i=-:tegra~ed s·:s:em ir: tiH•
I space sin-:.·.!--~tion ch.-+.n;bt"r
dt~rinL Q·:a! SA
/
Sheet_B-l- of ---
' '
QIJALIF!CATION STATUS LIST ALSEP PROGRAM CTc;TRAl Sl ,\T!O'; l'l ,.,. ·, nn::Ic S
CO:\!l'Oc-;F:" IS
~ ; 71 I ··-·-!-- . --~--~\1 ' ' ~. -
·•lrr'n ,T,), , ! .1~~-------·-~ -- --- ·---- -·
I1~'n1
~·~1n1enclat~re
( _':-- .:;ta ~1d
?~·~ e:·:er
Bx.-\ •2330523, 5 ~; I I. Fli~ht 2-A
SA Qual, S/N 4
170 12
E.:n'> lfuDll•t nt and I ()r
Paranwh.:r
L:-<VIRU~M~:',; fAL Tcn.pt.eraturc:
Operating
!\on-Operating Earth r,.!Jon
Pressure Operatmg !'on-Operating
Humidity
Operating I'on-Operatin)!
Vtbration Opnating ?\ A !\on-Operating
Launch & Flight Lunar Landing_
.Sire~~ Lt\~·1
Req_HirL·n,._·nt Capabdity
-10°f to +140"f-i·l0°F to tl40°F
-o3''F to+ 160''fJ.6S°F to tl60°F ':'>;/\
1 x Io-12 rnm llxl0"5mmllg
Sea Levd-!O"ti, m lxlo· 5mml-ig
lS~o- lOOa-o
')et..' Appcndi-...: A
15~, • 1 OO')'o
'//A , OG - peak 20 - 100 cps
Ac-celerati.:m ~~ /:\
Operating ':'./A ,4-.;- 1 min. l\un-Operating .>TR-16, Add. 1 0~ch nf 3 ax<·s
Shc·ck ~I A 0?Pra.ting \: ',-\ ZOG - 1 Orns rise
~~-O?erating ATR-Io,.•dd.•• e;chof3ax<>s
Agc·nl
Philco·Ford
\''
\'~,_·nf11 ;ill"n ol ~tr,·:-~ 1 1 ._ ,.J Cilp,thdLty
L1.Jtatiun
Palo Alto, California
Dt.•cunoen! Rt.'ft>rcnt·e
Qualification
Test R Pport RN-DAJ664
1\.
VI
Datl·
March 1968
--·- -- ----- . ---~ ;
Ren:arks
\lso q·.<aiifit·d ',11 ~ ~ ~ r(·tt'l:rt
n•ents tn Q•.1al S.\ test
Qual~f:~·d in Systcrn to S x I~~-· Torr<>
?\o tf·s~ing rPquir€'d a! s-. .;:tt•1z1 Ie\·el. QualifiE"d as a ~ubas~f'rnbh·.
OJ.al:fieC a-::;. rt o: ... ., ... 't•!ll
fur S;' l' 111 )Jr ·,. __ ,, I. t·: '
Te::;t i:-1 thP Sto\•;ed
Conft_·•.Jra~ i')!l • Q!..H l S:\
I Sait ~.pray :\,\ ~ t r Sar.<.i ;. Doo\ ::ot !J,.;,,.,, ·! • ~1.-\ I I --, 1 I I F,cr•2 .• s ' .\ ?\/A l ------i
Ae~,_ ... ~ttcal ?~uis(: ~:1,1 D1·!-lJH'd 1~/A __l
~:~.:; tp~~:::._ ... c :.rt
Ra1n ' ' >l/A Radtation I '\ \ 1':':/A
-·Explusion Pruof '-;.-\--:;/A PARAMETRIC
Pf'r~"H:l'la~JCf'
Spt·Llfl,-ation
F,_.~::ctional
Perfor:nanc~
E:vl: Pf"rforrnance
Per AL1!0700
Te.«t(·d a .. Jt•ct of Intf"gratcd Sy~tPr'":l 1:1 Spac~ Sin1ulation C:han1bPr.
_L I
Testf'd As ;)art of Integrated Systen1
l
Philco- Ford
BxA
llxA
Fa lo Alto,
California
Ann Arbor. l\1ichi~an
l
Qualification TP.-:t RPp\~rt RN-DA 1f,•·--!
TP z:nJo>z ATR-60, 70 BSR-230. 237•·
TP 23>30H/ ATR-27, 33 BSR-2300, 2320
~.!arch I a,_,o
!\fay-Jc.ne jgc8
-:-\ <' ~ (' ..: ~ ! ·-. r c> ; r f', ·
Pl:ii.:~· Fnrrl Q·;,a l
Qual S.\ test
Qual S.·\ test
Sheet..--.!li.... of
QUAliFICATION STATUS LIST-AlSEP PROGRAM Fa •'' ·-I j '· ']" · ['~, --=l 'J ., I ,.--,. ,. •'t\, _, •
.\nal)~t J.t..L ,.~ -." CF;-.lTHAL STATION ELECTRONICS C0l\IPONF"1S
Item !" utTiencla tu re
<..'on"'.n:;an~ DecoC.er
l'h.\ =2.' ,,_);(h)
~ >· ~
?li:.!!"-.t Z-A
SA Q-;a I, sj;o-; 2
HC-12
En\.· i ronn• ent
and/or Parameter
C<V!RCJ~<:--!EC\TAL 'I er::--.?~:.'rature:
Operating
Stress Lt:v~_·l
Requin.>n'.cnt Capability
0 t' -22 Ftu•l;~ F
0 0 -2l F to +15~ F I N,·n·l'p~rating I 0 0 I _ 0 0
Earth-t>5 F to +lbO F-bS F to +160 F M >un ;; '-\ :S I -\
Pressure Operating l"o.n-Operati!'_£
ft•stcd in Spare :-:.irn. Ck1n1bcr to
Hunlllilty
Operating Non- Operating
Vibration Operating Non-Operating
Launch & Flight L'J.nar Landing
1 :x 10-ll tnn,J!..:
"''Lt<~lxlO!:n:~H}:;xlO-t1 T~)rr
'.;I_!>,
I:; ... _, to lOO~o
Lk ~i~rwd to nH'L't
l! un1idi tv Relaui rcn1t.'nts Ie~ted to SV#l
\;/A 'Dt:tiJ.gnLimitTes Refer to ATR-16 Le,·els Refer to .\d(lt·ndurn I fit.; ;_ae s l through
Vcrificatlt..'n of Stress Lcvt·l Capatnlity
Agent
Bt•rulix At·rosp.tct·
Bendix .Aerospace
Bendix Aerospace
Bendix Aerospace
Location Document Peference
rp 2334335 \nn Arbur, MichjATR-•-0, 70
Bc;R- 2363, 21/h
.''-nn Arhor, Mich' PSR- 23b3. 23i6
AnnArbor, l\!ich~ N/ . .1,
AnnArbor. ~1hhJTP2;34~-l6
ATR-~2- R3 r;sH-2402. 2403
Date
May-June pi_,f;
\!ay- June
1%~
N/.:\
Ju':le IO~R
ragt..• __ ,,f ___ Fa ... , !"
Ren1a rks
Qqa}ifit'd ins~ =1 ch•ri:·~
Q lrtl S.·\ lt·ot
Test Li>,·el Li1~ntt·d bv Eq~liprT'.t·nt C:\r:-,:.,ility
~~J lt.>sting n"q·.1ire-d.
Qu;~lifi{'d to f"\·si:::n Li it Test Lt·'.els :or _')Jbp ..._ :... , ._:,· "'l (:: t!·e s~owed .. : n:i:::·:r -~i •. •1l
!urint: Q ... ll ~--\
Qu-.lif:t'd ~o l•t. ~:.::·1 :· ·i·.
July 1?68
Acceleration j f•·stt:d to I~=' ~~33434.3.
~perattng. ':~:.--: 14:tl_~l~hn_Dur BendixAr-roP.pac.e AnnArbor,\1h' _ .. ~TR-..,Yn,'_. 0 1 I J~lv ~--::-~stL~\-clsiN"li? ~-~!J;'J-Operatlng · .. :·~1~-' r: 1 -.·.:-~'PSln.\ ·s 1 ~R--4~;, Z-~1! }J,_.S lj..-.t-t·e; s~, ....... ~·: ,-.~r:.- .: --1
Sr.ock :t·:--~t·dtu l .1 1 ,_:_:,;.;,j._d Operating .-\ ± 2 ~ 11 n1s SJ.v .. ·- Bendix Aerospat:e Ann Arbor, ~Hch .\TR-~r. ~~ !\on-Operating _\ ~·-!t· -\~~'1. l tut•t'"' )t~:o.1E:>!:)i:lA· s 1~,~~-2--t·)•-. 2--tn"7
c_:::~tllf:cd ~o ~ .· Test Levels ior ...; ? , :
S,1lt Spray I~ :\ I . 1 .\ I H('ndlx A\•ro~<"-"ll ('
Sanrl f.- D·1 ~ t F11r.c•1s Acoustical 1'\oise Rain Radiation Explosion Proof
PARAMETRIC
Functional Per fonnance
EM! Performance
. \, ·: ···<! i)c·--1 : t-.:-..lt·(•t
'-;'.-\
:\ ,: :)!'TiLd
.-'. :'~ t A
•t ~ 1 P ~ iiH ri I. H. 130 w/ftl
"/A
ft•St('d as part ~~f Integrated Systen1 in spac l'l Simulation Chambt:>r
Tested as part of Intt_,grated System to A L 770 000
n1•11 \!X .\••1~<1~;> II'
I~t"Hii"'< Ac~ ro .. t\ lL't'
!':t~-;1rlix Ae ro!--p.(t ('
HPnrlix Ar ro~p...,r:e B<·nrli.x At.~rosp:1ce
Bendix Af!rospace
Bendix Aerospace
Bendix Aerospace
-\;-~ A r F;--;-y:·-. -\ll, ~
\nr .. \r 1 r!", \::,
:'\nn Arl·or. \h~,.
·\·~, .\r''•'f, ~,:1\
.-\n11Arl•or, },~)(-~
AnnArhor, :O.!hCI; I' 2334335 Ann Arbor, !>.-He:
Ann Arbor, Miclol fP l33303l
\TH-60, 70 P.SR-l3b7, 237h
AnnArbor, Michl TP23330R7 ATR-27, 33 BSR-2300, 2320
:O.!;;y- June l'H•t
~lay-June l~t~{Qtnlifil'd ,·i::. I::!(·~r~H~·rl. '-.-.-~!·
Ii:ern1al Va~-·~·~:n Test :•Jr -t
S1n1ulated L·.::-1ar :>.tisSltlr. .j 1r•
Q>al SA
~,~ay- June J0h8 ISameasabn·,·e
Sheet~ o{ ---
QUALIFICATION STATUS LIST·ALSEP PROGRAM l'f·.:" l 1\.-\ L S1.-\ I JON ELECT RO:'\ICS l Ol\1 i 'Uc: 1.:\ IS n.lt\ 1 11 .\1 \' l-------,. .-\nalyst _r. ~~
Item Nomenclature
:ta Pr·,r!>'ssor
,~,.~\ <~~30j2l,
~ :-; ... f"!ight 2-A
SA Qnal, S/:-1 3
970-12
En\·l ronmcnt
ar.d/or
Parameter
Stress Level
Requiren1cnt AI. 310'·>00
Capability Agent
Ec;\"IRO:\l\!ENTAL 1t:r:-.p..;rature:
Operating -22''y tot I <;s''r I-2Z°F to +158°F !Bendix Aerllspace
!\ .•n -Op,•rating Earth ~1J..._~n
Pressure Operating !\'on-Operating
Humidity Operating !\'on-Operating
Vibration
Operating
-b~°F to +l8SuF ( ... n5uF to +185°F
' ·\
- 1 2 lx10 m~j~lg 'c\tn tn lx!O l">nfl;
':!A I ;O""., to lOOcr'o
~:A
[P,l··d is sp.tre '- hdnlbt"r to <;xio-6Torr
Dcsi;..:twrl to n1 et..•t h:1r:1idity
rt·qll:rt'lrtf·nts
rested to SIP ~1 Dt>sign Lin1it
?'on-Operating rJ,_('fC'r to ATR-16 'Test Levels. Re Launch & Flight \ddendum 1 ft•r to figures 1 Lunar Landi~ •hrn 5.
Systenl s Din Sinn
Verification of Stress Lt>vel Capability
Location Document Reference
T. P. 2331335
.-\n•1 Arbor. \1ichl ATR-60, 70 P."'n -.~ ~f1?, 2376
N'A
T. P. 23343~6 ,\TR-~!, R3 ,.,,!{- 2402, 2403
Acceleration l ITestcd to H ±I~ I I l IT.!·' Z O'·lol3 Operating '-:/A l Min Dnr:.tion .-\ i'J:-90, 91 :"·)n-Operating \ fR-16 . .-\(~..-1. l ;; t5_nlr•..;, i.'<l• A--d~. ___ T-~-1\- 2.-tl2.L.Z.DJ
S':c-ck- Ieskd to IS± 2~ J_ Jf.l'. 2.0'4'UI Operating ":\/A 11 ms sawtooth .\TH-Rf, ;7
. !\'on-Operatin 'T ~- 16, .·\del. I 1 tinws ea. A."< is. __ ·- I\SR ~ 2406, 2-107 Salt Spra·; •. · ·\ 'Ci/A Sar.d (_;, D.lSt ",, '- D•·ti·
F •r.e·1s :\!A Acoustical !'\nise : 1),. I '~
Ra:n --~-i~~--~~~·/rA~-----1~--------------------+----
Date
May-June
191>8
):-:,/fl.
June-July 196R
if
Fa~\ --· J ~ ' -
Ren1arks
Successfully tested rrwdel
on Oual SA rnu<l~l
Test le\·c·l Ln.::, 111 ent Cai'" bi l
No te-sting: rf'q\li red
_-_,,-Q('::,i,:.··
-! st·.· _, t::! < o:~;' _ :;;! ·: "::.
I
\ l y
_j.,-
f Raciation ,J, ,, .. ,, 1 :.o ,, , a~ JH Lam ===rr:·p-:-rn4ili-=l\!;;y-June 'c8 1 Explosivn Proof :\ t\; A -I
PAP.-\.METRI.l;, ·e Td.:)le 1
~ "t.'t B-"
E!>.II Performance
T·· :l(·d 1.s · ~·:--t S'}·stcrn in S 1.
Chan1ber
f Integrated Simulation
T~sted as part Inte~rat.-d Syct·tm
i
i l
r. P. 233303z .-\fR-6r,7o IlSR-231>7, 2376
TP23330R7 ATR-27, 33 BSR-2300, 2320
l\!.1 ;--J ;ne 1968
May-June 196~
fi~(·rr. al t:;t:r-.
"'i:!· "d.:- •
ing Q•.1a1 e>A
Same as
: l
above
t
: ·~< ~.
T··=-: ;· rl
~: :r-
~---· -~-----------~--------------~--------~----------~--------;--------------------1
Sheet-!2l_ o! ---
\\.. n.~t· ,:-; .. \ . ' P'· '-· !\ ·. '\\,,,1\'-'1'···· -,-7 I OUALIFICA TION STATUS LIST·ALSEP PROGRAM .. l ]\,- "'
An,1ly~tT. Fox I Page I of I Fa.gt.·s
Environn1ent Stress Level Verification of Stress Level Capability
Item and/or Docun1ent Rt>Jnarks l':omf_•nclature Pararntter R equi rcn1cnt Capability Agent Location Reference Date
Transn:itter £:'\\'IR0:"\~!£1\'TAL Ten:pcrature: Ann Arbor Qualification I -12 -71 Suc~.~f"s~fulh· q~!ailfieod
BxA • Z3·Hb00, Operattng -22'Fto +l''l'F -22"Fto +158'F BxA Michi~an Test Report at c0n1ponent l('vel
Qual t'nits, l\'on-Operating '
ATR 266
S/N 21, 23, 24 Earth -63'Fto +200'F -6S'Fto t200'F Moon :>;.A N/A
Pressure -l2 -5
Flh:ht 2-A Operating lxlO tdrr_ lx!O _5
torr BxA Ann Arbor TP 2345106 9-21-70 Test Le\'el Lincited B)'
!\on-Operating _,
Mkhican Equipment Capallllity Fli~ht Model i60tolxln tp,.,. lxlO torr s·;-.;u Humidity s.:':-i 27 Operating 95..-, at J.tO'F 95"',at 140'F B'xA Ann Arbor NIA N!A No Test Required
!\on- Operating_ ~1ichi~<tn
Vibration Operating Per Pet- TP2H5118 5-18-70 S"'e first rencark !\on-Operating T:\1 511 TM 511 BxA Ann Arbor. TP 2345104 9- 17-70
Launch & Flight ~.Hchigan
Lunar Landing Acceleration
Operating :\;A N/A BxA Ann Arbor N/A N.'A No Test Rec;l:i:-ed
Non-Operating r..1i'-'higan
Sl-. ,ck Cperatiag ?-~;A N/A BxA Ann Arbor TP 2345105 2-18-70 See- fl rst "'l"en-a rk !\'cm-Op(·rating .!..0..:~llnt5f'( ~Og pt•ak, }j n"l"!cc ~1id·d(!an
Salt Spray :; A l'\·A Xo T c st P.·:·r.:· .... -: Sand & Dust ;.; A ;.; A "<o ! . ~·- " F•.•ngus :":A ~rA :'\o f•:!"t !~·- ... Acoustical Noise ;-.;A ;.; A :'\'~1 ~ c ~ t F. (" :: 1'
Ha1n :; A l'\ A Xo TeFt Rf'n ·.··v·i Radiatiun :; A N·A !\o Test .R ea!:I :-t:.·d Explosion Proof '; A N A ~Q Test Ht.•G·:~r~·.J
PARAMETRl&;
Flln(.:tiunal Per Per Ann Arbor Qualification
Perforrnance AL--!10-!00 AL--110400 BxA Michigan Test Report 1-12-71 See first rerna rk ATR 266
EM! PPr Per Ann Arbor Qualification Perforn"lanr(:' F l'Und
Performance AL-.JI0-!00 AL-410400 BxA Michigan Test Repart I -12-71 Acceptable In A.-~ ATR 266 S}·sten1-level Te~t
-- --~---· -.. ·---·- ---·--... -· .. -·----·-- --~------·-·-
970· 12 Sheet...liL_ of ---
/
QUALIFICATION STATUS LIST ALSEP PROGRAM Date 3/5/71 F\o. :\T\t_ns;,, p{cv, t<t,. -·-
Analyst Bak., r I Page .......Lof --l.._ Pa~es •.
Environment Stress Level Verification of Stress Level Capability
Item and/or Document Remarks Nomenclature Parameter Requirement Capability Agent Location
Reference Date
ENVIRO:"MENTAL During dt':O:;I!n l\n1:.t T 'y tt•:o:t, Ten1pt!rature: Qualification thermal platp !"~:tyt•d for two
A2 Multiplexer- Operating -Zl'F to+l58'F -22'F to +158'F BxA Ann Arbor, Mich T~st R~port 7 July 1970 hours at 3'-"<:>ragf' tf~mp. of
ADC Non-Operating ATR 236 +l40'F. All C S components BxA•2' ''1000, Earth
operat(~d !Eat i~frtr torily. t-.1oon s;:; 7 Qual
Press~1re Qn.-dificat ion s " 11 Fli~ht lxi0-5
mm of lxi0-5
mm of ZA Operating BxA Ann Arbor, Mich Test Report 7 July 1970 T<>st l<>vel lim\tPd by
Non-Operating Hg. Hg. ATR 236 equ;pmt'nt caoabil 'ty. Hurr1idity N/A N/A Qualification
Operating :gt;o;o humiclity ·:•95'\', humidity BxA Ann Arbor, Mich TPst Rf'port 7 July 1970 ~;o t('st requir,~d.
~'\on-Operating fn" I cv,·Jp fnr I ·vrlP ATR 236 Vibration
Operating Per P<>r Qualification
I ~'\on-Operating AL-410300 AL--110300 BxA Ann Arbor, Mich T<>st Report 7 July 1970
Launch & Flight ATR Z36 Lunar Landing '
Acct!h:ration 14.0 (l's a ion;.! 14.0 (i 1 s dlong Qualification ' Operating t'al h of thr(•t• each of thr('e BxA Ann Arbor, Mich T<>st Report 7 July 1970
Non-Operating rtXt'f: st Prtd •. ax' o o! 'n~v. ATR 216 Shock 20 C>-pcak 11 20 G-pcak: I 1 Qualification
Operating mscc :::.a,dooth mEcc ~awtooth BxA Ann Arbor, 1\!ich T c' st Report 7 July 1970 :\on-Operating Dcr ~ ff.. ~'ITIJ- 8]!1) trol!l -~""ID-SlQ]} cTR 2"\f,
Salt Spray :'<,A " A ~,;o !rst r~·q'l:rt"~.
&~nd i,o Dust c; A :>-:."A :-:o tv~t r~·C'!:;t·--:.
Fungus c; A N A :-<o tt>f~ r.·a·~:r(·ri.
Acoustical Noise :\ A N 'A :-<o t1·f~ TP9,'!;Tt·~.
Rain " A NIA ~<o tf.>St r~·g'.!~f{·rL
Radiation :.;:A :>-:/A :-;o test requirt>d. Exp1osiun Pro;:,f :\!A N/A :\'o tt_,st req_u:red. PARAMETR!~
Functional PPr Per Qualification Performance Al-410300 AL-410300 BxA Ann Arbor, Mich Test Report 7 July 1970
ATR 236
EMI I Per Per Qualification Performance AL-410300 AL-410300 BxA Ann Arbor, Mich Test R<>port 7 July 1970
ATR 236
-..
970 11 , .. Per M1L-STD-810A Sheet~ o£ ---
QUALIFICATION STATUS LIST·ALSEP PROGRAM CE'ITRAL STATIO;-.; El.ECTRO:-:rcs C0~\1'001!-::-lTS
IDdtC 3/5/71 I'"' AT\\·":·' 1F· '. '- '• J~r.alyot ~1 Fa&~ __ of ___ 1-':~c• s
Item Nomenclature
Power Distribution L"r•:t .PDl"l
'.hA 2'3'•4~0-2
sj-::, l 0 Flight 2 -A
.'>A Qual, 5/:C.: 4
970-12
Environn-.ent and/or
Parameter
El':VIRO:\~.\ENTAL Ten~yerature:
Operating !'\on-Operating
Earth :t\L'~ .. ..1n
Pressure Operating Non-OperatinJl
HJrr.idity Operating ~on-Operating
Vibration
Strcs~ Le\·cl
RequirenH~nt
-22°Fto +158°F
-65°Fto+I60°F
"' .\
Capability
-22°F to+ I S8°F
-65°Fto +160°F
_12
1 ~st~d in Sp.1ce lx 10 mmH~ ISit~nll. Chombcr S-/Lto lxlo-l-nln1 to ~xio-6 forrs
H" IDesi~ned to meet :J/ A !-hmidity Re-I:;·,..) to 1000""0 quirements
Operating t:J/A Non-Operating Refer to ATR-16
Launch !< Flight \dde:~dum 1 Lunar Landing
TestedtoS/P•d Desi~n Limit Test Levels Refer to fig I thru 5
Acceleration Tested to 14 Operating ~/:\ ± lg 1 h1ir". Dur-
l :\em-Operating \TR-16. _.\dd. 1 :":'"· ;t:mesca Shock J,_-~'t.·d to 1 S
Operating ~;' :\ ± .2~. 11 mo ::iJ.w-~;on-Opt:rating ·\TR-16. :\del. t tL'C_t!: 3 tirncs ea
Salt 5?r''Y t; .\ I'·; .-\ ~Sanr: j •• O·;st [~·•t D('1L1ed ~)•·:;:t:~1ed tn ~1··Pt'
Ft....ng•1s -t:\ "'l.'A
Aco~:.stical !\oise [;( ~ D~:fi·1o;.>d
Rain [; A N;A
\'-.·niicatiun uf Stress Levt>l Capa0illty
Agent
Bendix Aerospace Systems Division
Ccndix Aerospace Systems Division
I
Location I
Ann Arbor. Michigan
Ann Arbor, Michi~an
Document Reference I
TP 2334335 A TR-60, 70 BSR-2367, 23761
TP 2334335 I ATR-60, 70 BSR-2367, 237&.
;,fA
TP 2334346 ATR-82,R3 BSR-2402, 2403
TP 23J4S.f3 ATR-Qf), 0 1 ~~;o;R-2412, 2413 fP ~J3-i328 A TR- 0(·, 0( I BSR- 240 6, Z-l•c7
Date
May-June 1968
May-June 196q
N/A
July 1968
July 106q
July-Aug 106q
Ren1arks
l. Qualified in ~P" l d•.trin~ Q;;al S:\
Test Level Lin1itt!d by Equ1.ptne:1t C D'~:!it\·
No testing required
Qualified at St;bpa.ck,,~c(S P•·: i
Design Limit Test Lnch ic r a Stov.:ed Cor.flgUrhtion rl...:.rin~Z.Q_:.n1 ...;. \
I
~ ~~0 tt'<:tin:? ~' ':·:·r,,r:
~0 tC"~:.t-i-;-: TC'J'::r•. ·'!
~adiation_ rot Defined tested to 130wift~ fR I I I I I Explostvn Proof < ':\ ... ~/A
PAR!c!\:ETRIC
F·n~c ti(!nal PPrforrnancc
EM! Performance
T(•sted :1.s part {f lntcc.ratcd SystPm in S?ac,J Simulation Chamber
Tc>l<•'l as part t£ Integrated
Syst"'m t" AL77f 000
BxA
BxA
Ann Arbor. !\Hch:l~rtn
Ann Arbor, Michigan
TP 2'133032 ATR-60, 70 BSR-2367, 2376
TP 2333007 ATR-27, 33 BSR-2300, 2320
~tay-.Tune
196q See first ren~ar}
See first re
Sheet~ of ------
QUALIFICATION STATUS LIST ·ALSEP PROGRAM CENTRAL STATIO:'>! F:Lt:CTRO:-.:Ics CC'~II'O:-.:LNlS
rD"t'3/5/71 r:~~-~~~~-:-.--r~··· l\
F\nalyst J. T:f Paf.:t.' --"f ___ J ct'-,!e!-
!terr. >:orr.cnc la t..J. re
:'ower Co:1di:ion ... l:":k; •.·:. :?.C.~·. I
233Co,:.C-3,
S ·:-; 9, Flight 2-.-\
~A O~al, S,-:\ 3
9;"0-12
Environn1cnt
and/or Parameter
Stress Level
R equircnlent AL 410100
Capability
Io:C\ \' !R Oc:~.a;;>;TAL _ 2 2"F tu + 1 'i~°F -2 2 °F to+ 158°F
Agent
Bt..•ndix Aerospd1...t.
Systems Division T'""P""ature; o o o o I Operatmg .~; Fto+I~O F -65 Fto+l60 F J ~<-·n~Op~rating
Earth ~!.·,•n
Fr<·ssure 1::;,.,, L,•,·d to I l'<'St<·d to I I Operating Ix!0-ll Torr 5xlo-b Torr ;>;em-Operating
Hunoidity I I Desi~ned to I I Operating meet humidity :\on-Operati~g 15 to LOO_~a rcaui rerncnts ·
vl~iratu;n .\TH.-16 Tf':-.tvd to I · " S/P•l D<·si~n Operatmg .-\dden. "I L' -
1. ·re<'
liTH S ~ \. ]':on-Operating Levels(Rder to '!
La•Jnch & Flight Fig I thru 5) Lunar Landing '
Venticalilm of Stress Le\·(·1 Capability
Location
;\.:,;L i't T;.h.,IT J
~lie h.
Document Reference
r. P. 23H33; ATE-60, 70 BSR-2167, 237(,
1. 1~. 2.) J4 ~ b
ATH-60, 70 FlSR-2367, 2.376
N/A
T. P.llH346 A l'H-82. ~-~
BSR-2402, 2403
Date
l\Lw-June 1968
N/A
July I•lt.B
Ren1arks
Qualiiierl :r. 5·,l~,~~a~-~a~l·
~"l !iyStt!nl le·. t·1 tt·~ts
perfortTH•ri on t..::·:al SA
1 t.:~l lt:n~l lHTllt•:d fJj 'I!. ~t Equipment Capab1llty
Testi::g >:•,)t P eq\:i re-d
QuaLLI;;'c!. at S, ~ :~a~·:-:a~f· r'-1 L'l•·::-1~11 t ~n~.;, 1 • ::-t J.,·\ t.'l..:
~or 1 stG'-\e . ..: ~ ·1-::·::-J.r~-1:;...:·~1
in Qc:al SA
Acceleration .\I H-16 Testt•d to I T. P.l334343
Operd.ting .\d•i•·n.•l \hl~,lrpin ATR- 0 0,qJ l)ulyl%8 l"l[)es;£'' .J:" .P;·a· ~:c.n-Operating uur.t! . .t.m. ""tnnt'~ ' DSH. 2-+l., :411: : . J
\'e:·i:.ier1 a! S ·. :.'a.cf.:.a~e
Shc.ck ,\ rR-lt:o rest,·d to I i T. P.ll34328 Operating ,\d•l.-n. "1 l <-t 2~, 11 ms ~ t .\TR-86, 87 July 19(-8
·,·f::-::ie-1 a:~. ;:a. ~-a,:e
Desi~:; .~:r:;-:t ·:-t~s! a·,: C\.m-O;oerating l t1!'1es c.1ch P..<;J< _ ,~
salt'S?~ay :; .. -\ -;-.; 1:\ J ~r.J ;,;, D;J.St "\. !J, 1! ~., --'=.- _J__ -.!. .•0 .c~:. t·c .;~,.,:
F.n~J'lg ~\/·\ KIA
~c··us_~ical_...!_'::_oise I C\vt Ddnwd 1-;-.;yp I 1 :,, ! ,.,, 'c '• ·: Ram -;-.;, .-\ ~ill
I Radtatiun I:; ,t QdtnJ•d I I'>YD I I I I I I Exolos1on Proof ):ot Dt->flnt'd t~ I A ~ET.R.&
Fu!"!ctional Perfurn1ance
E~!l
Performance
Tested as part (11 ~ntq:::.rated System in Space Sin 11lation Chamber
Tested as part •·4 Integrated Systt>m to AL770(ooo
BxA
BxA
.·\nn Arbor. !<lie h.
:\nn Arbor, Mich.
T. P. 2333032 .-\TR-60, 70 BSR-2367, 2376
T. P. 2333087 ,\TR-27, 33 BSR -2300,2320
~fay- Tune-1968
~tav- !une 19l~
See first ren1ark
See first remark
.-Sheet-'".l.l - of ----
QUALIFICATION STATUS LIST·ALSEP PROGRAM
!tern 't'on'lenclature
Env i ronn1ent and lor
Parameter
RSST SYSTEM El\V!RO:\MENTAL l3H77 -001-01-01 Ten,pcrature: BxA 2 338511 Operatmg , !'\on-Operating
5':\ 002, Qual Earth
Stress Level
Requiren1cnt Capability
-22•F to +Jss•Fi!ZZ•F to +l58•F
Verification of Stress Le\ el Capability
Agent
Gulton Industries
Location Document Reference
Albuq., N. Mex.l 13877-992
~te 3/5/71 l':o.ATM-9Rf> Rev. 1'\o.
Analyst Lee Page __ l_of __ !_ Page•
Remarks Date
I '13/70 Note 2
-6s·F to +~oo·F 5/:\ 005, Flight 2-:\ !\bon I I I J J Not<> J 1
970· J2
Prcss~re < I X I 0 -I 2mmllc < 50 X I o- 2mmrrnl Gulton Industries I Albuq •• N. Mex.l 1 3877-992 I I !13 70 I Note 2. 1\ote 3
Operatmg _ R ''1 !\on-Operating Sl. to< 10 nnii
Humidity Operating !'\on-Operating
Vibrat1un
Operating !'\on-Operating
Launch & Flight Lunar Landing
Salt Spray Sand ~~· D~tst
F'!ng'JS
~1cal 1'\oise Rain Rtidiativn £yp)osi(Jn Proof
~!ETRIC
'0 ~. 13 to lC:o-··
n a ~l. :t
n.a
a_ a __ -na !)_ ':"<
n.-
as g-ivPn in
\t!L-1-Zio'·OO. and XASA MSC-ASI-'0-E:.ll -lOA
as ciYP~ in .\UL-I-.!ff 00. and :'\ASA :-.!SCAS !'0- F.~.!l-1 OA iS('L' r:otcs.)
::OTES: !. z. 3.
Certifrate of compliar.L! and Culton test Th('se l''n\·ironments \'-T e verified by Gul The s eci!ied "req'..lire ·ent'' levels were Gulto on 12 January JG 0.
I .. ---+-
Gulton lndustriPs Albuq., !J. ?\1C'x I 3P.77- 994 '21 70
Note 3
T'\ote 2 Testing perfornH"'d a! Sparton S. \\·., ,\Jbuq .. N. !\lex.
0-"ott"' 2 Te~t:r:c ?t'rfor:~;pr1 a: AETL. I ... A .. Cai::orr;a
Testinc pl•rforrnt'd at ~ta nri. Electronirs. Chicago. [JJ •
ata on (il\' to verify catahiHty _2
on Industries on l/13 70 toQTP l3R77-9l'2 exce;>t press:nl: '>:hich was telted to 5 x 10 mrr.!lg. ot required to bt• vt•rifjPd by the Culton t.sST qualifiratior~test per agree~ent at the QTRR held at
Sheet BIZ of ---
. ~
QUAliFICATION STATUS liST-ALSEP PROGRAM 1'.-xssrn: st:rs;.nc r.xPF.RI~!ENT ; ) l ~ ~ 3/;., '7 l
Analy~t
,p .\.r:-~:\t\. ~-· 1 I" ,
Item !':orr.enclature
J>Sr: Ser<sor .\ssf'mblv ~·~..:~~4~=
BxA • 23-!1604 S,':\' 1-502. rli~r.t 2 -A
SA Qual !31-H·-l~
S. :--; 3 & 2
Q7Q.)2
Env i r .. Jnrn~nt and/or
Parameter
E:"\\' ;Ro'<~!E="TAL Ternp~rat"J.re:
Opcrattng :-<l)n-Operating
Earth ~.1 JOn
Press·.1re Operating ?\on-Operating
H~tnidity
Operating ;-~. ·n-Operating
Vt:....ratum
Operating
Stress Lt•vcl Verihcatiun of Stress Levl·l Capabihty
R equircn1ent Capabiltty Agent
107° to L'.5°F Test~d is ~pace ~o:;°F to lt>!)°F ::lttnulat1on I Bend1x Aerospac£' :-'.tnu• as Ch,l.mlw r Cor S'(Ste l'llS Dn 1. sion
Opt•rating Ten1perarurc
1 x 10 ·l ~mm Hg I Vertfied to
I lr-R II <;xJO-<;Torrstn
x ) rnrn g ~;)ace S1m. Chan'-
?\ot applicable ;o-!Ou~R.IL
;)l'signed lo 1\!eet Humidt ty ")on 111 rPrn,.>nt"
""\Pt :\pplicable I l'C'st~d 1n Stowed Hefer to :\TR-ll· Conf1gnration to
Location
Ann Arbor,
~11.-higan
DocuinPnt Reference
T I 3022 TP23H335 A TR-60, 70 l\SH -Zlo 7,l37(;
1 N/A
TP2334H6
Date
11 ~:-an 6'1
June l OJ l%!l
~lA
6/28/68 0 · ATR-82, 83 !-<on- peratm~ .\ddendurn 1 \'tbration [)eS\gu nsn- ~-j0~,:'-10< Launch & Fhght 1.; 1._.,, hvhc.,t.:rl +------Lu:oH Land:_:.'JL_ i 'J.· ,, TP23HH3
Pa~e __ ,,f ___ Pa,e.t.~
Ren1arks
~ucccs ~fnlh· tt·~te-"i on lh~A Uua1 SA r-:-... u,:t'i
Test level lim1te-:l by test eq';ipn""ient ca-oabilih·
"' ·\ See iir'3t rPI: ark
-------------------------~---
7 i-t/6 8 Ac~ii;:;~- . . r~sted ,., St"wcd ATR-··r, I
0 •. :\otArpllcablt> (OtL(<e'lratJ,mt·) J)SR-'-l)2J-IJ5. -+-:pera.tng ·~ . , -----
!'~Cin-Operating \ TR- 1•1 .-\d L 1 l·l ± 1··. ~. ~.1::-'l. I Pl3343~H 1--h. - . I,.,,_,•dt:t.>t,;wed \!R-'>h,51 6;24;6il S .. nck ',ot -.mLg·:ral:<•n to ' · _
~e(~ firs"" rt·•· ar'.t:
Sr·P first tf·:'::'i r;... ('·,crating ·, 1 , 1 JS ± z, lln" I>.'> -• 4· ·,2 1r, ===t= ------
~ ~.~~i:~- ;tt: i";~ ==£-----~--------.Acv.l~tlcal :'\oise , ....... , \
Rain Fa<itation -~·:)~~i;:111·;ddr ---------1---------1 Ex .. lusion Proof :~ut :\~)~h a' le -----~·-. ---~----------
.fARAMETRI~ L u -+-- -F· . .~:---.ctiur.al ------·-
Perforrnance
F::',H
P~·rf0rmancc
T•~stC'd as part '1f Integrated Systt·m in Sp~c.'.' Sitnulation Chamber
Te~t··•l ao.; part (if intl;'grated ..;ystc·m
BxA
BxA
TP 2333032 ATR-60,70 BSR-2367,2376
-TP 2333087 ATR-27, 33 BSR-2300, 2320
I June 10 19<o 8 See first rer:lctrk
I April 196R See flr!'t re,~·a.rk
She<t__8.1_ of ---
~ -~. - ... . .. -----···"""' . - -..,..,.~-----------
r)ale 3/5/71 QUALIFICATION STATUS LIST·ALSEP PROGRAM PASS!VIc SEISMIC EXPERIMENT
JAnaly;:;.t
!tem
!'omenclature
PSE Central Station .Elt''- tronic s
B~.\ •2~34~-~_l
S,':\ I, Flight 2-A
SA Qual, S ·:-; I
Environrr.ent and/or
Parameter
£):V!RO:--.-:-.IENTAL Tc::n'perature:
Operating l':vn-Operating
Earth l\! :~""~n
Fret: sure Operating !':or.-Operating
Hum1dity Operating !':en-Operating
Vibration Operating !':on-Operating
Launch & Flight L'J.nar Landing
Acceleration Operating ~:~n-Operating
St-.ocK
Operating -:-<.-..r-:-Opeyating
Stress Lt.:'\·cl
R equircnH!nt
l07°F to 12S°F -b';°F tel lbn°F Sarn~ a5
C'pe ra ti ·~~
Capabllity
Tested 1s Space Simulation Chamber for Temperature
1 x IO.:j_nnn II~ I \',•rifiesl !c>
1 x 10 .smm Hg 5 x 10-"Torrs in Soarf' Stm. Chan,
!'>t't .\pplicable
:\ot \pphcable !~eft."r to.-\ TH.-h. .-\dd~ndum I
"ot Applicable -\ r;\ -It-. Add 1
:--~ot
.-\p-;-Jlt.·al,}p
! :' -I•·. \dd. I
Designed to ~Iet~t Hun1idity
I I\e.(h.:._.:.renu:.nts
rested l n St~)Wf'd Con:1g•.uatton to Vibratlun I1e~nt-:n Lt!:1lts fnd1catc>d in Figs. l Thru :;_
Tested on Sto\VPc!
Confi~uratllln to 14 ± l £! 1 ~,;,:1.
rc<>tt•d ln S;O\\'{'(~ •. :on:•~-trallC"'n tl)
l s __ ± .:u 1 ~rn.:; ~ : li:"'t' :' ! .1. •• \ '\::
Vcnficatiun o{ Stress Lt.-.•el Capabtbty
Agent
Bendix Aerospace Systems Division
Location
Ann Arbor, M1chigan
I
I
Document I Reference
-----fPB34335
ATR-60, 70 I BSR -2 36 7, 2376
!'> 1.-\
TP233-IH<>
ATR-82,83 BSR-2.J02,2-103
TPZ> 34 343 .-\TH-~0,9!
PSR .2~ I 2, 2-+13
TP23H128 \ TR -'>f., ~7 DS R -~..;0€-. 2407
Date
Jun<' 10 19b8
b
N/A
6/Z8_u8
7 /.J/6 8
6/24/68
-F''·' AT\!-~'''· J Fa~::t· __ ! --- Pa~··:-
I Ren1arks
I Successfully tested on BxA Qual SA model
v
C\ i c\
Sarc ... ·ssiull;. T{':3'.··d. U::c!~ :---:-.
Successfully Tt'sted. Q· .• sl :--\
Succe~sf:.:.ll._.- ~~s~··::. 'J . ..; ....... · ..
~ Sal• ~?:-ay ~" D·1!'it
F :r~ .-\c .... J...lStical :-;uise
:-ti ,,,
~~i I ·;Jl .... ,:.ohh· ,~·", ~~~',r~·;,,;~~ ·-tl-------+1---+1-----~1 ) ~!:, I '
": _• 1• ' !.; ·-!. ~ ;J)•lr·
970-12
ham '·ca'olt• ~ \pplj,a;,J.c__ F:aC~ativn 1), ··+JlCdtoi\!ce
t;;:xplvsiun Proof r-:ot .-\oollcable £0ARAUETRIC
Fu.r.ct;.onal ?er!ormance
£;\!! Per!onnance
Tested as part I>! the integrated system in the :-.hace simulation chamber
TestNl as part p! the integrated systcn\
BxA Ann Arbor, Michigan
BxA Ann Arbor, Michigan
TP 2333032 I June I 0, ATR-60-70 196 3 See first re-n~a rk
BSR-2367,2376
TP 2333087 I April ATR-27, 33 1968 BSR -2300, 232n
See first rerr~ark
She~ t .Ja:i_ C't ----
··'
!Date 3 s 17 I 1:-.:o. !Rev. :-.:o.
QUALIFICATION STATUS LIST ·ALSEP PROGRAM AT~!-O>b
!Analyst I Page of Pa~es
Environment Stress Level Verification of Stress Level Capabihty
Item and/or Document Remarks J';ornenclature Paratneter F equirement Capability Agent Location Re(erence Date
S h r CJt~d, Thermal E};\'JRO:-.:i.!ENTAL Earth Sciences llu!(hes Aircraft Engineering See Note Below Cor:~r'-)1
Ten1perature; Divisiqn -Teledyne Space Siinulation Report No.
p :--;233,016-501, Operating -300- +250'F -300- +250'F during DVT thermal Laboratory 640-0263-0053 S Feb. 1968 S :-; IU, Flt. 2-A !';on-Operating
vacuum tests El Segundo, Cal. Earth 1-.L•on
~.\Qual Pressure
Z334A67, Operating I x IO-I 2
mm H!! I x I0-7mm Hg " " " " s/~; s & 9
F N0n-Operating SarTl.e as opcr. Humidity Designed to Mecl
Operating :\ot arpltcable Humidity Non-Operatine ~l'-·-lrr·-r<. H. ~~l'l 'tirt•rn.-nt5
Vibration H;:g3
;Ht. Bunker Ramo DVT Report Operating Sec Rcrnarks 23 -'·' \). Jll4 Earth Sciences Corporation ENY -R -Z363 Nov. 1967 Non-Operating 58-IOO 12cbloct Division - Tcstmg Lab
!00 -200 0. 39 Launch & FltgH
~~g=·ma~~~cJ9' 1 T eled )'TIC Canoga Park1
L mar Landins; Coli f. Acceleration : :c•t app!i .. ~a blc
O?erating 'I " " " ..
!\on-Operating H _A 14 g 1 > Shuck 20:..:± 10 l
Ope·rating ;'>:ot apoLc,hle ~:1'-t: tnoth lll r--:1 F('"l: ri f:e .,
" " .. !\' .. ln-Operat~ 21'± 1 ,. i "' .. •' . "' .
Sa.lt Spray '·' t ,... "'"')• 1: .·:l\ 1' I\: • on•X ·ohl.• Sar.d & D..1st -~~o .1 .c: "" .. F·:r.£!115 ,. •I "' ·" ,., '
' '" ·--1--·-----~-=--=-~ Accustical Noise ·: lt a•v)l:,·c:t!)lC' :-;ot annLcable Rain :<ot ao~)~:.:ablf~ :-;ot annlicabl• Radiatlon l'C))_<;?) h.<; on.•..!•~ Explosion Proof :-~ot aoolicable Not aoolicable '
PARAMETRI!;;
>OTE: PSE Shr" jld qualified on Su package •1 in~tallat101 j per tc st and cport references hown on SP# 1 Shel't n 1.
970-ll ~
Sheet~ of ------
QUALifiCATION STATUS LIST·ALSEP PROGRAM Date :\,J. JR,_·v. ~u. ~
3 ~ 71 ~~ ~
Analyst Fagc __ ,.{ ___ Pa~t·s
Item l'omenclature
PSE Gnomon As SPm
BxA= 2 33801.-50 I, S,:.; 10, Fl:~ht 2-A
~A Qual 2BS016,
970-12
£nv 1 ronn1t:nt and/ or
Parameter
E='ViRO~Ml::l'TAL Ten:.r::erature:
Operating !'on-Operating
Earth 1\1__,vn
Frt·s~ur~
Operating l'on-Operati~
HtJmlrLty
Opt~ rating
1-- l'c·n-Operating Vib:ratlon
Operating l'on-Opera!tng
Launch & Flight Lt:r.ar Landi~_g
St rt..: S!- Level
Requirement
107'Fto 125"F -65' F to 160" F San1e as ope rating
X JO-J 2nunJlg
-S X 10 I1"!tl1H~
'-:fJt apnl\(·;1hlr
:-;,,t anplicab1c Reft·rtoATR-16 .\ddendum 1
Capability
T" sted •n Spau• Sin1ulation Chamber !or Ten)perature
\. ,. rificd to 5 S. 10-;TOQfS iP. ~'):-\,.!,Sip~. C!l~n
·), 1._'n ·I to
~kPt Hnn,idltv l' t~~:·ti r,~~1wnt ~
I ~,;st~_·d in Sto .. ,·~,.·rl Configuratiu;, to Vibration ne~ign Li1nit~ Indi.catcJ in Figs. I thru 5.
Agent
Bendix Aerospace Systems Division
Verification of Stress Level Capability
Location
Ann Arbor, Michigan
Document Reference
TP2334378 ATR-160 BSR-2570
N/A
TP2337905 ATR-149 BSR-2546
Acceleration Tcst,,d in Stowed T P2337915 0 · , 1. .. , , S :\hshawauka,
16,
peratmg . ;\ot app tcable Conttguratton to B"1 D ::odiar.a ATR- __ .. ~.?r.-Operatlng .\TI',-lb, .\drl. 1 14·!:1".1-.!in. BSR-Zot{
::,;;.ocK ~\tJt lc~tyd Pl ~tc;v.·ed Bendix J\prosoact... Ar~n Arbor, rPZ337917
Date
12/30;bK
N/A
12/19;'6i'l
1/15/69
I 17:69
Remarks
Successfullr Tested at Svsten1 Leve] as a Result oi Qual SB Test Prograrn
):,A
Suc:::es:;:fully T£>sted at System Level as a Rt'S'..~lt
of Qual SB Te~t Progran-:
Oper-ating arpla:able 15~ 11~' 1{j'11~~~ 11 to Systen1s Divi;ion !-.1ic/-:igan :\TR -16_1
I- l'c•C":.:_<_?pcrating .\1 ;: -Ii· Aced. 1 1 ··!'-:", •·:" !\•·u BSR -25 tl ---+·----------------i Salt Spray ~r)t an·)lu.:abl('" 0:t'l. arol:.::ablf'
Sand & D·Jst ILE·'-;"o. . r),,,;gnedtoi\kd I I I I I ----j F· .... r.£_•.s ""<ot a:'":l~l:cablf' :-\ot annli,~abl.-. ,:,__{.(_,; ~-tt< al r-;visc I· .ut illl~~~l=--~~~~i~ht, ..
Ratn t------------------f---------------+---------------+-------------r~--------------------------1 ~diatiun _ .. E~p}? __ sio_fl Proof
PARAMETB.ll;_
Sheet~ of ---
QUALIFICATION STATUS LIST·ALSEP PROGRAM
ltcn1
Nomenclature
Solar Wind Sp,'ctrometer B"A •2330658 Flt •I S/);.8 =-,. --? S!!\;-9
Fit =ZA Sr~-1 SA Qual, S, N 6
970-12
F:nvt rr)nnH'nt
and/or Pararneter
E~:VIFO);ME);TAL 1en-.pcrature:
Operating Non-Operating
Earth MJon
Pressure Operating Non-Operating
Humidity Operating Non-Operating
Vibration Operating Non-Operating
Launch & Flight
Stress Level
Requirement Capability
- 300' F to +250' f1-300' F to +250' F
-65' F to +160'F l:-iot Yet T .. sted _',[)0°f:' tn +?t;O""'d_'l.(JO"t=' tn +Jt;() 0
Sf•a LP\'('1 -1 (1-12 Torr
l'i - !OO"j
\A
LT.l\-8
Tt•st to 5 x 10-6 Torr
N,'A 15 - 40"",
Lunar Landing I L fA- 8
Tested in Stowed Configuration to Design Limit
Ll'vd lndkatt•d in f"igUTPS 1-'J.
Acc~leratton
Operating 1:: A Non-Operating
sha<:k Operating Non- Opera tin~::
Salt Spray Sand ;, D•;st
:.TA-8
.• A :..TA-8
A .-\
);ot Y<'t Test~d
LTA-3 D R
Funcus 1:. A
Acoustical Noise L: A Rain Radiation
1-::-~osion Proof PARAMETRIC
Functi0nal Perfonnance
A ;_;:D-520 130w .. ft2 ~. A
T£>st.•ri as part oflinte-grated system in Space ~imulation Chamber
EM! Performance !Tested as part ofjintegrated system
Agent
BxA
BxA
BxA
BxA
Bl\!SD
BxA
BxA
BxA
BxA
Verlfi .. ation of Stress Level Capabihty
Location
I Ann Arbor, !-.1ichigan
I Ann Arbor, 'di<-hil!an
Ann Arbor, :\!ichil!an
:\nn Arbor,
I
Document Reference
TP233303l ATR-60 PCD "'"
N/A
TPZ334346 \~1cl:in~,n __ _gR-RO
~-tishawauka TP2334343 I Inr!iana
Ann ArLor, TPZ3343Z8 I ~!ichigan
/Inn Arbor, Mich.! 2334335
TP 2333032 I ATR-60, 70
BSR-2367, 2376
Ann Arbor, Mich.! TP 2333087 ATR-27, 33 BSR -2300,
2320
IDatt> 3/5/71 1-c--~~--~----~,
:'\:u.AT\1-u:-.r· ~Rt..'\'. 7\u.
!Analyst T Pagc __ of Par.:~·s ~
Ren1arks Date
ll\!ay 1968 I Qual SA Test.
BxA facilitif'S will not allow May 1968 testing to bPiow 5 x I0-6 Torr
(Qual SA testl
!\'o t~sting: planned to N A I oor, Je,·ei
June 1968 Design Limit Tr·st.
I July 1968 I Design Limit Test.
I June 1968 } Design Limit Test.
~!a 1968 Qual SA Test
Qualified contingt.~nt 8;7 .:68 on P. I. re,·ie"· of SW<: data.
I 4 il 9 60
Sheet....!D.l_ of ---
QUALIFICATION STATUS liST-AlSEP PROGRAM ' JDate""{_....__ 71 F\'\)·AT"t-cl)-.r· . _p~t'V. !\" .. _\.
jAnalyst I Page __ <>{ fagt:s -Stress Level Verificativn of Stress Level Capability
En._ ironment Item and/or Docun1ent Ren1a r-ks
!\ on1enclatu r e Para1ncter Requirement Capability Agent Location Reference Date
Lund. r Sur fa(_ c }~;-~VIP()~\ ~dENTAL
~~at.:. nctometer Tenlperature: Tested in tni~:don
BxA o2330657 Operating -oOO'Fto2SO'F TP23H345 Sin1ulation Testin~.
F}(o}S·;\0-3 Non-Operating Not Yet Proven BxA Ann Arbor, June 1968
Flt , 2 s ';-.; 4 Earth -GS'Fto+!60'F htichigan A TP.-60, 70 Mvon _300'Fto+250'F BSR-2367 237(1
Flt ·2-A 5/~ 7 Pressure I o-12 Torr TP2333032
SA Qual, Operating Sea Le\·el 5 x 10-
6 Torr BxA Ann Arbor, A TR-60, 70 June 1968
S1N.!. Non-Operating Jo-12 Torr r-lic hi)!a n BSR-2367 2376 Hum1dity Designed to mPt :'\o testin~ planne~ to
Operating Humidity Ann Arbor, 100-· Je,·el. Non-Operating 15 - I 007o Rcaui r€"ll)cnts BxA ~.1ichi 'an ::-<'A ~'A
Vibration Tested in Stowed Tested sto\Vf"d - durin.: Operating :-i'A Configuration to design limit tPst.
Non-Operating LTA-1 DR De"i~n Limit Ann :\rbor, June 1968
LannC"h & Flight _·\TF 16 Add I L,,vds lndkate•l ?-.til hi!,!an TI'23HH7
Lunar Landing LlA- J D. R in Figs. ! -5. BxA -· Acceleration T!Jl1,3-+3-!3
Uperatlng :~ A Tc•tcd to 14± l~ HI\ lSD ~ti~ha\ ... ·aka, /\"lF'-'~0.91 July l9t·8 Te~ted stov.erl- d~Jri·•t.:
Non-Operating ATR lb Add I 1 min Duration l·~diana BSR-2412, 2413 desi~n lin~it tc•st.
Sh•>ck Operating ~; A T~st<•rl to 15±lf! A.,n Arbor, TP23'412" June 19t-F- Teste~ stowPd- r!'.Jri'"':::: :"on-Operating .\TR 16 l'.dd 1 1 I ms Sawtooth Bx:\ ~'~ichigan A TR-~(·, 1'7 desi~~ 1in1.it test
Salt S;)ray ·;.A S:::.n.-J f~ D·; bt .. ·\ F·~n~::us :.; A --Acousttcal 1'\oise :\ .-\ --.Rain :; .\ Radiation I.F:D-520 130w'ft~ BxA i\nn Arbor 1\licl: 2~''i4335 Ma·I068 Qual 5A Test Explosion Proof ~.; A
PARAMETR{!:;
Functional Tested as part o integrated BxA TPZ333032 June 1968 Qualified contin"ent on I'erforman{.e "ystC'nl in Space imulation A TR-oO, 70 resolution of l·H-132,
'~ham her BSR-2367, 231~ Di ~ita 1 fi.lte r rn.a Httnc tion in LSM
EMl Tested as part o BxA TP2333086 April 1968 Performance integrated systcn A TR-27, 33
BS R-23 00, 23 20
-
-
-970-12 Sheet-illL of ---
.-QUALIFICATION STATUS LIST·ALSEP PROGRAM- A;;SF:\!IILY Sl'I1PACKAGE Hl.
~Date 4/24 '70 ~No. AT~t-",-:;' IRev. ~l,,
jAnalyst J Page __ uf --- Fagt'!;
Item ?\"Qm.enclature
pa. ka~e 112 2x.-\ .233-j(hO,
s :\ 15, Fl,c:,t ~-A
SA Qual 23484Q, '>. '•; l
•7: 12
En\·ironn'lent
and I i.JT
Parameter
E!'\VIRO'\l\!ENTAL Tt;"nlpt:rature:
Operating Non-Operating
Earth
l\L'l'~n
Pressure Opt! rating N•m-Op,!rating
Humidity
Operating ]\;on- 0_llera tirl_g
Vtbration Operating !'\on-Operating
Launch !. Flight Lunar Landing
Acceleration Operating !'on-Operating
Stress Level
RequircnH.>nt Capability
(l "1 0 "'--3QO Ftot2;o -300 Fto+27011" -l·5°F to +lt>0°F (See note 11
- 3<10°F to z;o"r I -l00°F to +Z<iC'IF
-12 ltl Torr
-12 :;T, tr> 10 Torr
Y.'A 1 =:. -1 ° 1' ...
:\'A :? pfer to
CF 10fl•l"l
'\ A CTl"•l OUl
Tested to I -(J
~x111 Torr
Designed to ~feet lh:midity I llcqilite' Tested in Stow~ Configuration tc
Desi£:.n Lin".it I Levels Indicate
Fi~Jlres I 51 Tested to 14.:_ 1.: ea.._ h axis
Agent
BxA
fix A
nxA
13xA
[lxA
Vt..•riftcation of Stress LevPl Capability
Location
Ann Arbor, ~Hchigan
Ann Arhor, ~tichb . .!an
Ann Arbor, rhi ~~an
Ann Arbor~ Michi~an.
Ann Arbor,
i-.1ichi: .. 'an
Document Reference Date
T PZ 33433 '(E'\V'•
TPZ333032(1ST\ I b/!0/68 ATR-bO, 70
J'.SH-23(,7, 2371,
San1e as above
N.'A
TF23343~8
ATR-84, g; l),SR 2-1-0·~. 240.;
TF2334J30 A'l R-oz, 93
b/10/68
N/A
6/28/68
7,1i../C.8
S!:.•ck le5~ to l~ "'-c; ... ,·:<·:Jnc .\ ., 1
.- T11
l3~·~~~l ,.
Rema:rks
Qualllied in Qual SA test progran1
Test level Jin,t:ed hy test equipment capahilities.
See first ren~ark See :\vtt: ,,c-l>l\V
3e-efn~~~e .,;~-
2c: each ax~ ;-:vn-Opcra.tin CPIC't•')'~J] .. ;eac.laXlS BxA A.~n!:r!n'"'r. , .. \-:-R-'38,8Q I'J/30'tl8 Salt Spray ·~·~"------~,,~,u·r~~~-~Z~1un~s~~z~~~~l~c~-----------·---+~~~--~--------------------J
. ,._, J (' St f~ cq :1 r'L'"1 ~ :~ I' (1 '·. ~I''~
.o .!. est ~· ('0 .: !"t:'l
~& D•!St I,.,~ ")rji:<·1 I I I " ",, Fung1S ~
Acousttcal Noise I '~·-~t.....J.....efi~~ed Rain Radiatitm Explc;SH•n Proof
PARA!\!ETRIC
FunLtional Performance
':' .\ ~.Eu- ;z·1
"[('stc•d as part<""·!·
an inte~ratcd 5":-·:-
tern in space sir· '.llation chan1:-.)er
13·1 w/f~ 2 I. R
Capable of DcpltJyrnent and operation on Lunar S~rface
BxA
BxA
Ann • .-\ r:-:-or !\,1 ichi~an
Ann Arbor, Michigan
See first iteln a~Jt·ve
See first itcrr ... a~~bve
~OTE:: ALSEP 5~ •2 with HF E S, ~;~z subscquentlr rfqualified for physical 't'vironments prr !f.·· Array D SP >2lQualification Test Plan, TM 593, RPv 13, Minutes, BxA}; . 9703B-26 dated 19 F bruary 1971, t),\:' Board Meeting ,fJted that the Array D. P .. z configurattr, was qualified co tingent on satisfactor>· loscout of actiunLtcinS.
:o :-est Hl•g :~rt::d ~':o :est if'qt:)!'t•'!
:-:ee li rst ret~ .u r~: ~<o Test Req·urt'(~
See first ret·~ar\1.
Sheet~ of ------
QUALIF'CATION STATUS LIST-ALSEP PROGRAM SL'llPACKAGE II, RTC; ASSI~I-I!'LY Date 3 5 i' l r: .. A:\·--·" r· . b t"\ •• ~''
Analy•t F.W i !'a C.\..' .. , ~-<.1~ ,. _ ...
En\· i ronrnent Stress Level Vcnflcation of Stress LL•-,..] CapaLtlity
Item and/or Komenclature Parameter Agent Location
Document Remarks R equi r-en1ent Capability Reference Date
EJ'\'IRO;'<MENTAL R.,dioi>otope Temperature:
QualihcdtlVn at 1.ssen1!J:\ lt" ··i
The riT';)C lee tric Operating BxA Ann Arbor, TP 2334335 May-June was performed by G. E. Re ~·e r
r;~;;,t:rator !'on-Operating I000°F to 1140° 11700 F 1\!ichi!(an ATR-60 1D68 to test reports ,\:0.::-Q
ti·:. -:-. G) Earth BSR-2387 Doc. :-lo. 6300-~81,
I\ bon -380°F to H0°F S00°F .\~SQ Doc. No. 6300-lRS
; ··.~E.. !r-l7£3(l')779 Pressure Sxlo- 5 torr
~.~od. 21 Operating Sea Level to Test le\·el limlit'd b'!-· test
";.; t32000&, l"on-Operatin~ • ln-12 16xlQ-8 toor BxA ~.\'i~n'~~l'.?r' eqtnpment t.:ap:tbility
flicht ~-A Humidity De st~ned to n1eet Operating 15 to 100'\'o humidity require N/A Nl:\ N;A N/A
No tt:>stlng require-d
F"d ,··'J'<Ulc, 1'\,>n-Opt>rating "it'tlfS
4 7l'l1l'l'400G I, Vtbration Gcnt'"r;ll Etc~ tric ~ '; t ~ ~ 0007' Operating ATR-16 Refer to Table I Valley For!!c General GE Doc. il~300 Qualifierl at ~~:!1pa.!·ka.12:e ?
Fii~~t 2-A Non-Operating Addendum I Technolo!(y Center Elect ric Doc. •6300-288 Jan 1968 Design limit lcvc'l in H.e
Launch & Flight Philadelphia, Pa. stowed config·.lrat:er', Q al -, .. \
SA Ql!al, Lunar Landing !1c:er to ATF -~-1. ~.;
~!od 15 Acct:leration Operating .\Tlt-16
7. SG 3 to 4 min BxA
Ann A rhor, TP 2'34330 each axis
June l9t8 Sue<. es s!ulh I ._~sterl, Q·...:al :-.; \ !\on-Operating \drl(>ndum I
\~i.chlgan .-\·: :C-02. qJ
Shock 15 G each axis i Operating -\ TR-16 BxA T!' 23~4331
t:on-Oporating .-\d<lendum 1 11 msec± 10% ATR-~8. go ~~\.!;'.(' J. u i.:8
H.·· '-2 0-' 2 0' Salt Spray :; '.\ :'-;'.\ N/.\ ~ .\ "'.' Sand i: D11st ·;;n c; E - ·u~.· o. '""' :--IYD Fung•1s 'I \ Ni 1\ Nl.-\ N'.\ Nl.\ .Aco·Jstical Noise ,-n NYO r.-.: PI d p,. .. :-JYD Rain "' \ N/A N .\ N/-\ N/A Radiati0n 'iYD !\!Yn r. <' Ph' PPn NYn '":'t>e line 1 Explosion Proof :-IYD NVn r: J;' Phil PPn< NYD
PARAMETRI!:;
-
__ ...... Sne .. t~ o! ---
J).lt' S'_. P PAr·KAca· tT. R TC SlH'R T!~(", P:.~·c. UUALIFICATION STATUS LIST·ALSEP PROGRAM ' 3 ~I
Analyst
Item l'ornenclature
• : 1.:J ::-:-orting
: )~\!;:! .-\ ~:;·y
:-··xA z:,300li, ': ~.
Fli.:ht Z-A
ee ~>:rte l.
SA Q·~al 2335520, sit-: 1
970·11
Envi r ... ~nn1cnt
and/or Paraineter
E:\ \: IFo:-:~!E!\:TAL Tt!n1Ft.:rature:
Operating 1'\on-Op.,rating
Earth Moen
Pressure Operating :'\on-Operating
H·Jmidity Operating ~on-Ooeratin2
Vibration
Operating Non-Operating
Launch & Flight Lunar LandinJZ
Acct:leratic..n Operating ?\on-Operating
Shucl-: Operating ~ ::.r.- Operating
Sai: S?ray Sar:d (;. D·1st
F":cg:cs Acvustical Noise Ra1n Radiation Explosion Proof
PARAMETRIC
Stress Ltvel
Rcquiren1cnt Capability Agent
Bendix Aerospace
-300°F to +50°F ~-300°F to +L50°J-I System
-o0°F to Ho0°F -b0°F to+l60°F
l :<1 0- llTc•ors ~Lto lx!O-ll
:-;!A
XIA
'l.e'cr to Fig. 1-5
Tested to ';x!0-
0 Torrs
Llt:"~l~l.ed to m~E""t Humidity Rt>quirem('nts
rt'sted in sto'.\~d configuration to Ot'Sit.!,n Li111it h-vt.~ls indicated ·,y Fig. 1-<;
Vcrlficatton of Stress L·~~-el Capability
Locahon
Ann Arbor ~Hchigan
~/A
,\nn Arbor ~tichig<tn
Document Reference
TPd34335 TPL33303Z .-'\ TR-60, 70 BSR-db7, 2376
If
~·A
TP2334348 ATR-84,R5 B;'H-2404. 2403
Date
JUiw 11&8
':-II A
July 1968
: ~ / • .l..
LT-\-3D'R
• 1.' :-- •. \ d t 0 1 4 ± l ~ l rni;:; duratin:-:. TP2334330 June l9b8 -:..~i"''('~ ,;: a'":!:-; _.1..Tg_oz. q~
t!~tcd ~u l-- :t 2!2 2 5.)4351
:' '.\ :1 rn~ t:a\\'.tHlth '.'1i:-~",·~9 -1 U.ne 19t8
!. '_\- 3 :J 'p •in;t~..- ~~~ a"ls. '':-;tz -240~. 240" .\
: ~ ·~ :),. :";.:-:.(· d
:' ·\ :<ut D(·rirn·d :; '.-\ ~~()t Dt·:"ined !R l30W/ftz ~·\ /.\
!'\ate 1: Quali!itd on Qual SA confieuration as R:<,.-\ 233<'~~ .-\ssembly ReY:I;ioh C whic;, i identical to Bx.:J l338017 Assembly use4 on Array B and
-.'·L-,:.,.--..~:;i~ .. ~!'"'---no<--:~-----
r··\i\·-·-· !··'· ', Pa!!"_. --~! ---- i'a&.:t'~
Ren>arks
Sllccessf~llh• :~sted
on Qual S.\ model.
Capability li:o•:tc·d l,y to·st F:quipnu•nt Capa.h1i1ty
No testing required
5uccessfulh· Tcs•ed, Q;.al s,~
-I ,.•
She.,t___llll_ of ---
QUALIFICATION STATUS LIST·ALSEP PROGRAM S\.:BPACKAGE •2, APOLLO 1.1':'<".·\R lL\l'llLl~~G TOOL IALI!Tl D.ttt: j S I J f"\il). A T\1 ~'} ·" • p~ t'v, 1\~•.
!Analyst .1 rs I Page c>f Fa~'$
F.nv i ronr." ent Stress Lt::vcl Verification of Stress L~:vel Capab11ity
Jt.,m and!or Nomenclature Agent Location
Document Remarks Fa ran1t:ter Requirerr1ent Capability Reference Date
El\:VlRO:\"l\1ENTAL ~-.. ~-F7 Ten1r-crature: See ~otes Belo''-''
"'EB V41 Jll65, Operating i '" "1005, l\:on-Operating I di,<ht 2-A Earth
I I
J\lx,n
SA Qual, Pressure S:·:-; l Operating I
' ]'lon-Operatinl! Humidlty
Operating I I l'>on-Operatinl!
V1bration I
Operating I Non-Operating i
Launch & Flight
L1m~ r Landing I l Acceleration
Op(;rd.ting
!':on-Operating Shock
Vpcratir..g ~:, __ ;n. Opr.:rating v
Salt Spray Sand & D·Ht F lDE'.lS
Acvust1cal 1\oise Rain Radiation Explosir.Jn Prou£
PARAMEIRl~
;--;ote I: The A .HT mass simula nr rather than a ight configuration mod I was used for th
Bx..-\ Q ·al SB system le' '1 dynamic tests.
Note 2: Refer o ~p- 2 QSL Shee for shock, ~ibration and accelerat on environment
levels ·.vt . .:l. appl\· to l mterlace quallll· a lion.
-
I I I I
910-12 Sheet...lUL. of ---
===::c ..... """""""""'·"·'"'"""""'"'""""""""""""'"'"""
QUALIFICATION STATUS LIST·ALSEP PROGRAM !Date 3/8,71 j:\u. A I ;\I OHt jRc,·. ;\u.
11-'l,'t~¥~~ Brent I Page __ of-- Pagt•s
Itenl Nomenclature
f'Si·: LeYelin~ Stool Asst>mblv p;;; 23HOQ BxA •23->4723, S/:\ i, Fli(!ht 2-A
SA Qual 2335945 5/); I
970-12
E:Y.-! rvnn,ent and/or
Parameter
£;\\'IHO::ME!"TAL Temperature:
Operating !';on-Operating
Earth }..1.)on
Stress L•:v<>l
Requirement
I 07 F to 12'i F -~5-F to 160 F an1e as
Ppe rating
Capability
fes!ed in Spa,-e Sin-n1la t ion Chamber for Temperature
Pressure II x lo-llmm !11.:1\'erified to Operating I x Io-Rmm H~ 3 x 1•>-STnns in }:on-Operating "Pa<"P Sin~. Ch~~rr
Humidity I l!'e•icn<'d to Operating .~.:ot App1i('abl,. '.'_!PP!. I!unlirlity !'\on-Operating __ ~ .... a~:i rcnW''t ~
Vi'::Jration :\o~ Applh-ahle Tt>sted in Stowed Operating :'~efer to AT R-1 b Cor.figuration to r-:on-Operating Addendum 1 \'ihration D~sign
LauJ>ch & Flight Limi~s ln•licated L·1nar Landina 1n T-'i>•s-. 1~1:;.....,..
Accclt:ratlon I 1Tes~ in Stowed Operating :":at ... -:-oniie_l! ra~ion to !'on-Operating .·\')pli .... a~~lC> 1.4.±_li!_.l '.rin
Shock . ~:<ot .-\p?li' a:,le I Ps•~;·rl in ~·owt.~~! Operatlng ·\·: ;{-}t·-.\·:,l 1 1 .~:m ra'Ion to ~on-O:~erating l "">7":;, 1 .•• } \rr;s.\v;c:
"':c1• .-':.,o:Jli,·a '\le
V,·rificativn "f Stress Level Capability
Agent
BendLx Aerospace Systems Division
Location
1\nn Arbor, Michigan
Document Reference
TP2334335 AT R-60, 70 BSR-2367 2376
N/A
TP2334~-<8
Date
May-June 1968
I N/A
11 T R-84, 85 I July-Aug BSR--:'.404, 24<JS 1968
TP2334330 AT R-92. 93 7/4/68
TP233433! AT~-88, 89 6/24/1:8 F\S R-240R. 2.400
Remarks
Qualification Accomplished at the System Level. QS.o\
! I I ;
~~~~~~~------~'--! ~-'-------l-~~~~~--~~----------------------+----------------+----------------+-------------4-------------------------------1 :o· .'.Jpli· a·)Ie .o\pnlJ, ,,:.1•· __ ________ -~-~--------·- -·-
1 Acoustical Noise _'io• /\pph~ a~·le Rain '\ot A D:>li<-a '>le Radiation I L!.D-?20 ll'esi~ned to :..lee: Explosion Proof ~-:ot Applk .. -hle -- !\o_t-~p_li<ai>le
PARAMETRIC
~ I I I I I I I ---1
Sheet~ of
QUALIFICATION STATUS LIST-AlSEP PROGRAM lDatc 1 5 '71
'Analyst JTS lr-;o. - r AT!\i-0$6 Rev. No.
I Page __ of ___ Pages
Item t\onocnclature
H e·at Flow Experir:--...... ::.t 2145-J.30, ·' :-.; {l,
Fll~:,t 2-A
~:3 Qual 2330661, s :-; 3
ar.d s;J Qual 2345430, s :-; 2
~
970- ll
Env i ronrncnt and/or
Paranlt~ter
EKY!RO);!\!E);TAL T~n~pa.:.rrtt•.1re:
Operating !'on-Operating
Earth M.•vn
Pressu:t"e Operating t-;on-Operating
Humidity Operating
!\'on- cpe_l'~!i.ro& Vibration
Operating !'!on-Operating
Launch & Flight Lunar Landi!lg
Acceleration Operating
he =--:on-Operating ~~1'·' K
(•f·t·r;t~i--:g
1\on-Cpnrating Salt Spray
~nd &_Dust F·~ng'JS~ --
Stress Level
R equi ren1cnt Capability
-300'F to +2SO'f1-300'F to •250'
-65'F to -160'Fj!'ot Tested -300'f' to "~50'
S ~a Level to Jo-12 TORR
1 5 to 1 oo·~
N/A
LTA-3D/ll LL\-3D/R
:\.A
Sx 10" 7 TO!l.R Desi~nt .. d to 1\!eet Humirlity R equi ren1ent Tested without failur.: to le,•f>ls
-.h '•\T In f]Q!i.ri'S
1 - s:1, 1, 3, -1, :;, ~:...rr?.v f)
ATF-!c ADD. Ill~g ±I"., mil"~
;-;'A l~.:..:-2~; ~a'.\tC'~1tl'1 15±;:\! .~awtoot~l
... \ ,\,A
:: A
Agent
BxA
BxA
BxA
BxA
BxA/B:-.lSD
BxA
Vcriflcation of Stress Level Capability
Location ' Document Reference
---Ann Arbor, I TP23Hj87 Michigan ATR-160
BSR-2570
TP2H-!387 Ann Arbor, I ATR-lbO !\: i chi G!;!' BSR-2570
Ar.n Arbor, J:\iA ?l.fichigan
TP2337905 Ann Arb0r, ATR-149 ~Hchigan BSR -2546
~!ishawa1.1ka T})2337Ll J 5
lnJiana ATR- It-t B<:H-2~74
TP~3379 17 Ann Arbor, I ATR-li.J 1\:it..:hitan BSH -2571
Date
Dec 19 68
Dec 1968
N/A
o~~ J9t,q
Dec !9 t3
Jan 19r.g
Remarks
Qual SB Test
BxA facilitif"s will not allow testi~g to below 5 x I 0 TOR P
No test required
Qual SD Dt:>sign Lln.it I t>st
Array D .. SeE> :--:otP 1 & 2
Qual SB Design L:r.1it Tt>~t
Qual 58 :1~si£n Arrav IJ- .St'«' ~~( .. ·~, 1 ~ ~
Acoustical N'oise I :~.A
Rain Radiation Explosion Proof
PARAMETRIC functional :Jerformance
:.;:A :>:,A :>:,A
Test<'d as part systen1 in the cha:nber
of integrate<! Space Sinlulatio.
flxA Ann Arbor, l\Hchigan
Tl 0 2f3,(-!0 i!\lo•J. IST) ATR-U·3 BSR-2573
Jan 1969 Qual SB Test
l:"ote I:
~ot<.> 2:
Sj:; 02 'f'bsoqu<'ntly n·qu.lified on SP"2 as nott>din Array D Qu~lilcat!o~ As.s .. ss':"e1' R":view Boarr M;n 11tes 971J3B-2i, dated 19 F<'br· orv 1971. TP 21 1(.32R is th .. docum,•nt ' 1\'o•nng th~ Dn11·, Ltmtt VJbratton '"stmg for Si-' 2 Array D, and TP 23.;; ~9 is th<· docunH·lt covC'ring the ShoC'k r q~tirt·mt·nts of Sl' 2. Array D.
Design 1 ::>it (x, y, z) with t '" s. N-2 HFE on Arra D SP"2 were pe or~ed January 1p11 at the foiiotdng levels: ~· '"' ~ . / . _. . •"• ~ - -~ . - - ..
b. c. d.
L f.lB random ( J. 0 mlnl Lun r descent randoml(12. 5 min) Shot.¥ (l 5)
3.0( 37. 5( o.o
IIIJio
min. min. min.
Sh.,et..li.:.:l__ o{ ---
~._,,
CUALIFICATION STATUS LIST-ALSEP PROGRAM Date 3 ·s '71 r•o. ATM-981> IRP\· .• No.
Analyst I Page of Pages
Em,.i ronn1cnt Stress Level Yerif>cation of Stress Level Capability
Item and/or Nomenclature Agent Location
Document Remarks Parameter Requircn1ent Capability Reference Date
Supra thermal £]';V JRO:'\J\!ENTAL Ten1pcrature: TP 2333032
Ion Detector and Operating -300°F to +250°F -300°F to +250°!: ATR-60, 70 May 1968
Cold Cathode Non-Operating -65°F to +160°!:' BxA ~nn Arbor, Mich BSR-2367, 2376 June 1968 Qual SA Test Subpackage
Gange Experiment Earth -300°F to +250°F -300°F to tZ50°F #2 BxA 2338104, • !-.bon s.~ 7, - Pressure TP233032 Test level limited by Flight 2-A Tested to
"! Operating 10-1 2 Torr 5 x 10-6 Torr
BxA Same ATR-60, 70 June 1968 te•t equipment capacity
SA Qual 2330660, Non-Operatinil SL-lo-12 Torr BSR-2367, 2376
S/N 1 Humidity Designed to
1'\ o testing pia nned Operating NIA meet humidity BxA Same N/A Non-Operatinl! !5"1, to l OO""o requiremc:-nts
to I OO"'o level
- Vibration r csted in stowe~ TP Z3H348 Operating N/A configuration to ATR-84, 85 Non-Operating design limit BxA Same BSR- 2404, 2405 · June 1968 Qual SA Test Subpackage
Launch & Flight !C 314105 le\~cls indicated #2 Lunar Landing in Fi!,!ure-s 1 .. 5
Acceleration Tested to 14_t1g TP-2334330
Operating NIA 1 rninut c dura- DxA Sun1c ATR-'12, B
July 1968 0'1>1 SA Test Subpackage Non-Operating JC 314105 tiPn ~2
s;,,,ck 1 estell to l ::-..:_l.t: 1 p ~.l3-15Jl
Up·: r>.ting NIA ll ms sawtooth BxA Same A TR-88, 89 June 1968 Q·,al SA Test Subpackage :Kon-Operating !C 3H!Oo each axis flSR-2408, 240' #2
Salt Spray "i r\
Sand & Dust ;-.: i A :<ot cicfint ,1 .,o ~es 1:1~ Jar.ne(J
Fungus NiA Acc.ustical N"oise :~~~t dc-fi:1ed ~..:o Te~tin?: Planned Rain :\'A '
Radiation LED-520 130 W'ft2 (!Rl BxA Same TP 2334335 }.fay 1968 Qual SA Test Subpackage •2 Explosion Proof N/A
PARAMEfBI!;(
Refer to RAS 100 '.Rice Univcrs ity CEI Specification)
Integrated T P 2333087 SIDE S/N 2, Proto used
EM! Per!ortnAnce Teot"d as part o ATR-27, 33 in ASE EM! requal System BxA Same
BSR-2300, 2320 April 1968
completed I 0-19-69 per TP 2338180
Per RICE Tested as part TP 2333032
Functional Specification of Integrated TP 2333035 May-June
Performance System BxA Same ATR-60, 70 1968 See firot re ... ~rk BSR-2367, 2376
"""""' , .. Shee~ of ,
-----·-~ ~
~'~~~-- - -
