ALSEP reliability mathematical model & prediction

IIMDIX SYSTIMS DIVISION ANN ARBOR, MICH. NO. ATM 274 RI!V. NO. F

16 May 66

4 August 66 7 Sept 66

23 Sept 66

13 Jan 67

ALSEP Reliability Mathematical Model & Prediction

10 May 7 PAGE 1

The pages contained herein represent Revision F to this ATM.

OF

This revision represents an update of the Prediction portion of the Reliability Mathematical Model, Prediction and Assessment Report.

37

The pages contained herein, along with the unrevised pages contained in ATM-274, Rev. E dated 13 J;'. , 1967 constitute a complete issue of the Reliability Mathematical Model, Prediction and Assessment Report.

In accordance with the Reliability MCP this Mathematical Model and Prediction will be revised periodically throughout the program.

As the in-depth reliability mathematical models, predictions and assessments are accomplished and modified they will be incorporated into this report. This will permit programwide knowledge of subsystem and system numerical reliability status.

The detail prediction worksheets for each subsystem are on file in the ALSEP reliability office design and test history workbooks.

This publication represents the Interim Prediction and the Interim #2 Mathematical Model.

Prepared by ALSEP Reliability Group

Approved by __ ~-""~~...;c~=--..=....;""-,..._-·-=rt':..... .... _-_.__ S. J. Ellison, Manager

PAGE

ALSEP Reliability Department

r~n4f~ CORPI!)RATION

Dt:NLJIJI. ;)J;)It:M;) LJIYI::>IUN ANN ARBOR,MICH. NU.ATM 274 l'tt:Y.NU. F ALSEP Reliability Mathematical ...._ _____ __,_ ______ _

Model & Prediction 10 May 67 1d OF PAGE

LIST OF EFFECTIVE PAGES

Remove the following pages from ATM 274, Revision E dated l3 January, 1967

Title Appendix A Appendix B

1 A37 AS4 B4 B41 ld A38 ASS BS B42 11 A39 AS6 BSa B46 12 A40 AS7 B6 B47 21 A41 AS8 B7 B48 22 A42 AS9 B7a B49 2S A44 A60 B8 BSO 2Sa A4S A60a B36a BS1 28 A48 B37 BS2 30 ASO B38 BS3 33 AS1 B39 BS3a 3S AS2 B39a BS4 36 AS3 B40 BSS

B38a

Add the following pages: Revision F

Title Appendix A Appendix B

1 A37 AS6 B4 B42a ld A38 AS7 BS B46 11 A39 AS8 BSa B47 12 A40 AS9 B6 B48 21 A48 A60 B7 B49 22 A48a A60a B7a BSO 2S A48b AS9a B8 BSl 2Sa ASO B37 BS2 28 AS1 B38 BS2a 30 AS2 B39 BS3 33 AS3 B40 BS3a 3S AS4 B41 BS4 36 ASS B42 BSS

37 PAGES

BS6 BS7 BS8 BS9

BS6 BS7 BS8 BS9 BS9a

r~ncf~ CORPORAl ION 10 May 67

4. 5. 6. 3

4. 5. 7

4. 5. 8

4. 5. 8. 1

4, 5. 8. 2

4. 5. 8. 3

Dr;;;I''ILII/\ ,,,nr;;;m., LIIYI;)IVI'I ANN AKHUK,MILN, "'"'ATM 274

ALSEP Reliability Mathematical Model & Prediction 11

PAGE OF

Full Failure

Any information output less than that listed in 4. 5. 6. 1

Heat Flow Experiment

The objectives are to measure the temperature gradients and thermal conductivity characteristics of the lunar subsurface.

Suprathermal Ion Detector Experiment

37

The objectives are (I} to measure the flux, energy and velocity of the positive ions in the lunar ionosphere and {2) to measure the characteristics of the raw and thermalized solar wind at the lunar surface.

Full Success

F

PAGES

Two energy levels and one velocity level and a pressure measurement.

Degraded Mode

Any one or more of the following will result in partial success: a} two or more energy levels b) one energy level c} any velocity level d} pressure data only

Full Failure

No data from this experiment.

~~ncf~ CORPORATION

10 May 67

4. 5. 9

4. 5. 9. 1

4. 5. 9. 2

4. 5. 9. 3

4. 5. I 0

4.5.10.1

4. 5. I 0. 2

4. 5. 1 o. 3

5. 0

cr::nLJII\ .>J .> 1 J:M.> LJI YI;)IUN ANN ARB 0 R, M 1 C H. nu. ~r:: Y .nv.

ALSEP Reliability Mathematical ...,__A_T_M_2_7_4_---~. ___ F ____ _

Model & Prediction PAGE 12 OF 37

Active Seismic Experiment

The objective of the experiment is to determine the structur ep thickness, physical properties, and elastic constants of the surface and shallow depth materials on the moon.

Full Success

Four mortars fired and exploded plus twenty thumper squibs fired plus range and zero time data, plus three geophones.

Degraded Mode

All combinations of 0, 1, 2, 3 geophones plus 0, 1, 2, 3, 4 mortars or 9 through 20 thumper squibs.

Full Failure

No geophones and no mortars and no thumper squibs.

Charged Particle Experiment

Full Success

Electron and proton data in nine out of ten channels, plus all six veltages for a total of 61 days. This could be revised to cover the 61 days as follows: All Charged Particle data in an undetermined number of channels greater than 8 but less than 12 and all six voltages.

Degraded Modes

Same as above for: a) 3-10 days b) 11-30 days c) 31-60 days

Full Failure

Data in less than 9 channels or less than 6 voltages or operation for less than 3 days. This could be revised as follows: Data in less than specified number of channels or less than 6 voltages or operation of the experiment for less than 3 days.

Mission Profile

The mission phases used in this model include factory acceptance test through one year of lunar operation. Figure 5. 0 presents the mission phase/time profile.

PAGES

EQUIPMENT

V.lPrtl"ir;,l PnwPl" lA R, R\

Data (A}

Data IB)

~-

t--Structural/Therma1 IA&:B)

Passive Seismic IA&B)

1\A;, anPt()niPtPl" (A\

Solar Wind lA)

f-lp;,t Flnw IR\

c: lnl";,thP1"rY>Al Tnn nPtPrtnl"

-~ IAR,R\

ArtivP C:P; _,m;r IR\

CharE:ed Particle (B)

Svstem A l"rav A

Svstem Arrav B

NOTE: ALL VALUES IN UNITS OF 0.01%

970-8

ALSEP RELIABILITY STATU 5 RECORD

CURRENT PREDICTION PREVIOUS PREDICTION MNEMONIC GOAL

CODE ALLOCATION A PRIORI DATE A PRIORI DATE

PWOO ggoo g31g33 20 Mar67 . 98194 20 Mar 67

DAOOK 0 9642 . 87 064 13 Jan 67 • 8 r Ob4 13 Jan 67

DAOOL • 9642 . 86388 13 Jan b7 • 86388 13 Jan 67

STOO 0 9997 . 99256 13 Jan 67 • 99256 13 Jan 67

PSOO • 9900 .901297 l 0 Mav 67 . 93000 2 Feb 67

MAOO . 9900 • 85904 4 AuE: 66 85904 4 Au£ 67

swoo . 9900 .85427 4 AuE: 66 . 85427 4 Au£ 67

HFOO 0 9900 • 899297 1 Mav 67 L• 87747 20 Mar 67

TIOO • 9900 gqq} R1 Mav 66 ggql 11 1\A;,v hh

ASOO • 9900 gg6qq? I;> 0 1\A rtr _ _h7 qq_7oo ?n M;:n 66

CPOO . 9900 77305 11 .Tan i:J7 77_395 13 .Tan 67

SA99 gooo . 5046 hnl\ff;,vh7 S7.nh 1 Ll An,. {, 7 -.----

SB99 • 9000 . 4734 l1 0 Mav_..£7 _47_67 1 Ll Anl" h 7

Reliability Status Record Table 8. 1

DATE

10 May 67

CURRENT DEVIATION

-. 008116

-. 09356

-. 10032

-,00714

-.09!-370)

-. 13096

-. 13573

-. oqo703

-.0909

t. Q0699:Z

- 21AOS

-. 3954

C----

-.4Z6b 1

::J> 1-3 ~ N ...J 1-f:>.

:::0 (1)

< "I)

1:J Ill

(JQ (!)

N

0 ,...... VJ ...J

ALSEP RELIABILITY STATUS RECORD

CURRENT PREDICTION GOAL

EQUIPMENT MNEMONIC

CODE ALLOCATION A PRIORI DATE

Flie:ht Handline: Tool PWOl . 999950 • 999996 20 Mar 67 ·-

G~n~ratnr .A<o<oPmhl" PW02 .994230 • 994756 20 Mar 67 ---

Fnel Cao & Cask Ass'v PW03 9994 00 ' 999496 20 M<u 67

Power Conditioning: Unit PW04 0 996500 '987733 20 Mar 67

PC:U /PnU C:ahle PWOS 999900 999900 20 Mar 67

Tnt;:rl,; PWOO 990054 '981938 20 Mar 67

970-8

PREVIOUS PREDICTION

A PRIORI DATE

" 999990 l3Janf--.i

994750 l 3 Jart 67 f--- --

. 9994 90 13 :;d-, (;(

----- ~·

. 973160 1 3 Jan 67

9999 00 l3Jan67

-

. 9G7450 13 Jan 67

y

DATE

20 M<, r 67

CURRENT DEVIATION

+.000046

+.000526

+. 000096

-- '

-.008767

:!:o. o

-. 008116

>r-3 ~ N "'I ,.j::..

;>::! (t

<:

~

1:1 (lJ

(1Q (!)

N N

0 H;

V.l "'I

EQUIPMENT

Passive Seismic

Central Station Electronics Elec. Assembly Calibration Attenuator Short Period Elec. Power Converter "A" Power Converter "B" Long Period Elec. "X"

Axis Long Period Elec. "Y"

Axis Long Period Elec. "Z"

Axis Level Sw. & Trig. Gen. X Level Sw. & Trig. Gen. Y Level Sv,·. & Trig. Gen. Z Digital E1ec Module # 1 Digital Elec Module #2 Ditigal Elec.Module #3 A/D Converter

Sensor Electronics Sensor Elec X Y Z Axis Sensor Elec "W" Board Long Period PreamQlifier Short Period Calib. Assy. Long Period Calib. X y

& Z Axis Lon2: Period PreamPlifier_


970-8

ALSEP RELIABILITY STATUS RECORD

MNEMONIC GOAL CURRENT PREDICTION

CODE ALLOCATION A PRIORI DATE

PSOO . 990U 0. 901297 10 May 6

PSO 1-(0000) . 9934 0, 934023 10 May 6 PS01-(1000) 0.999850 ~0 May 67 PSO 1-(2000) 0.997748 10 May 67 PS01-(3000) 0,993580 10 May 67 PS01-(4000) 0.997693 10 May 67 PSO 1- (5000) 0.995266 10 May 6

PS01-(6000) 0.995449 10 May 6

PSO 1-(7000) 0.995478 10 May 6

PSO 1-(8000) o. 995478 10 May 67 PS01-(9000) 0,999992 10 May_ 6] P301-(9100) 0.999992 10 May_ 6] PS01-(9200} 0. 999992 10 Mav 67 PSO 1-(9300) 0 996269 10 Mav 67 PS01-(9400) 0,995711 10 Mav 6' PS01-(9500) 0, 996373 10 Mav 67 PSO 1-_{9600) 0. 974601 10 May 67

PS02- ( 0000) • r; 97 1 . 970194 10 Mav 67 PS02-l 1 000) 977821 10 Mav 67 PS02-JZOOO) 0 993563 10 Mav 67 PSOZ-(3000) 0.999683 10 Mav 67 PS02-(4000) 0.999961 10 Mav 67

~S02-(5000) 0 99.9.615 10 Ma\L 6' tp_S02_- l 11oo8\ 0 qgqi)R~ 10 M::.v h 7

DI\TE

May, 1967

PREVIOUS PREDICTION CURRENT DEVIATION

A PRIORI DATE

0. 93000 2 Feb 67 -. 098703

!

~ 1-j

~ N -J ..,.. !Jj (D

<:

1-rJ

'"d llJ

CJQ (D

N \Jl

0 ...., VJ -J

EQUIPMENT

Long Period Preamplifie1 Uncage Circuit

Electro- Mechanical Long Period Hor, Boom

Assy" {2} Spring Caging Assy. Mass Caging Bellows

Assy" {3} Gimballed Platform Assv. Upper Platform Assy. Boom Assembly Base Enclosure Assy. Uncaging Mech. Assy. Leveling Drive Assy. Leveling Stool Thermal Control Assv. Sensor Assv. Bubble Level Mercury Switch Assv. Short Period Vertical

Assy"

-


970-8

DATE

ALSEP RELIABILITY STATUS RECORD May 1967

CURRENT PREDICTION PREVIOUS PREDICTION MNEMONIC GOAL CURRENT

CODE ALLOCATION DEVIATION A PRIORI DATE A PRIORI DATE

PSOZ-(7000} . 9995 ' 0. 999683 l 0 May 67 PS02-(8000) 0. 999994 l 0 May 67

10Mety67 PS03-{0000} . 99460 9 10 May 67

PS03-(1000) 0. 999860 10 May 67 PS03-{2000} o. 999960 10 May 67

PS03-(3000} 0. 999765 10 Mav 67 -

PS03-(4000) 0. 998101 10 Mav 67 PS03-(5000) 00 997853 10 Mav 67 PS03-(6000) 0.999930 10 May 67 PS03-(7000} 0.999465 10 May 67 PS03-(8000) 0.999994 10 Mav 67 PS03-(9000) 0.999752 10 Mav 67 PS03-(9100} 0. 999998 10 Mav 67 PS03-(9200) 0.999998 10 Mav 67 PS03-(9300) 0 999946 10 Mav 67 PS03-(9400) 0 999998 10 Mav 67 PS03-(9500) 0. 999996 l 0 Mav 67

PS03-(9600) 0. 999967 10 Mav 67

Passive Seismic Experiment Table 8. 2. l-4 (Con 't)

I

> 1-:l ~ N --J ..,.. ::0 (!)

<:

f-rj

1:J flJ

(JQ I'D

N \Jl flJ

0 ,..... VJ --J

EQUIPMENT


Heat Flow Electronics

Probes

Reference Junction


970-8

DATE

ALSEP RELIABILITY STATUS RECORD lOMay 67



HFOO 0 9900 0.899297 l May o7 -.090703

HF01 . 9910 0. 902491 1 May 67 -.088509

H02/03 . 9991 0. 946382 1 Mav 67 -,042718

HF04 . 9999 0, 999334 l Mav 67 --. 0Qi)_56_~ -

Heat Flow Experiment Table 8, 2. l - 7

> t-3 ;s:: N -.]

>l'>-

~ !'!)

<!

f:rj

1:J [lJ

(JQ

'D

N 00

0 ...... VJ -.]

EQUIPMENT

Th11mnPr

,.....,P,"'' ;-; ''\'"'1 • ,.

l\A" ,-,,..t::>,.. P::> r lr::> rrP ~

Central Station Elect.

Total

.... 970-8

DATE

ALSEP RELIABILITY STATUS RECORD 20 Mar 67



ASOl 9999 . 999996 20 Mar 67 . 99996 13 Jan 67 +-,000096

AS02 9994 . 999889 20 Mar 67 . 99976 13 Jan 67 +.000489

AS03 . 9975 . 997686 ~-

20 Mar 67 . 99946 ,----- 13 Jan 67 1-.000186

--- - -- ---AS04 . 9932 . 9f)9126 20 Mar 67 .rl-1172 l3Jan67 .Y. 006226 ---

- ----· --- -- --- --ASOO 9900 . 996997 20 Mar 67 • lJlJbY l), JJ.r. (,', ~.006997 --

.... 0 .., ..,, ~. ~

l

Active Seismic Experiment Table 8, 2. 1-9

.

> t-3 ~ N -.j ..,..

~ (D

<: 0

f-rj

1:l Pl

(JQ

rc

~

0 ...... w -.j

BENDIX SYSTEMS DIVISION ANN ARB 0 R, M 1 C H NO. ATM 274

REV.NO. F

13 Jctn 67 ALSEP Reliability Mathematical

Model & Prediction

8.2.2.2

8.2.2.3

PAGE 33 OF 37 PAGES

Electrical Power Subsystem

An improvement in the over all reliability was ad:.:eved by a redesign which eliminated relay Kl and its associated components. This increase was achieved although a number of capacitors were added to eliminate single point failures.

Data Subsystem

This reliability prediction is for the baseline design configuration as defined by the delta PDR. The estimated reliability of the data subsystem was calculated to be • 87065 for array A and • 863883 for Array B. This prediction though still below the reliability goal shows a marked improvement over the previous reliability prediction estimates (. 8229 & • 8188).

The mcst significant improvements were realized in the areas of the command decoder and data processor. There was a reduction in the reliability prediction for the Power Distribution Unit.

The primary reason for the different prediction is attributed to two factors: standardization of failure rates for performing the prediction, and design modifications that were incorporated as a result of the failure mode and effects analysis.

~~,;~ CO~PORATION 13 Jan 67

8.2.2.4

8. 2. 2. 5

8.2.2.6

8. 2. 2. 7

8. 2. 2. 8

Kt:V.NU. BENDIX 5Y5TEM5 DIVISION ANN ARB 0 R MICH. NU.

ALSEP Reliability Mathematic,al ~-A_T_M __ 2_7_4_..L.... ____ F ___ _

Model & Prediction 35 PAGE OF

Structural /Thermal Subsystem

An increase in Reliability in the Structural/Thermal Subsystem was caused by the following changes and considerations:

(a) Compartment l structure has incorporated the single-forged unit in place of the sheet metal build-up used in the previous prediction.

(b) Use of more realistic failure rates for structural members where safety margins will permit.

37

{c) More complete Reliability analysis of all structural and thermal members.

Passive Seismic Experiment

The current reliability prediction is based on a full success criteria as defined in para. 4. 5. 4. l of this report. Although this estimate represents a decrease in probability of full success from previous estimates, this estimate is based on essentially the final design and on actual component stresses with the required adjustments reflecting application factors.

Magnetometer Experiment

PAGES

The prediction data contained in the GFE Contractor preliminary report, dated August, 1966, has been evaluated for mission success probability and the results are included in this report.

Solar Wind Experiment

The prediction data contained in this report were calculated from the failure rates presented in the GFE contractor preliminary prediction, dated August, 1966. These failure rates, when combined in the proper mathematical expression to represent functional operation experiment, indicate the contractor has presented data which predicts 86 per cent of the goal.


This prediction reflects the status of the Heat Flow Experiment at the time of the Critical Design Review. The predictions of the electronics, probes and reference junctions are firmly based on the current design and any change resulting from the CDR will be reflected in the next update. The model considers the two probes in a parallel configuration and. shows that the desired goals have not been achieved.

13 Jan 67

8. 2. 2. 9

8. 2. 2. 1 0

8.2.2.11

8.3

IIMDIX SYSTIMS DIVISION ANN ARIOR, MICH. "g. tn:v. ""'· ALSEP Reliability Mathematical

Model &: Prediction

Suprathermal Ion Detector

ATM 274

PAGE 36

OF

A first application of the Reliability Predict ion Model has

37

been received from the GFE subcontractor. This prediction model represents the first update of the initial apportionment. The reliability design goals have been established for the breakdown indicated on the ALSEP reliability status record. Bendix has not received any prediction data and cannot at

F

PAGES

this time include a current prediction, however, the goal allocations presented do represent the GFE subcontractors design goals as submitted.

Active Seismic Experiment

The prediction provided in this report illustrates achievement of the goal which was initially assigned for one hour of lunar operation after one year of lunar storage. A reorganization of the analysis has been performed to group the circuits by function and environmental conditions. A stress analysis has been performed for the majority .of the parts in their application and the prediction was adjusted to account for the application data.

Charged Particle Experiment

An updated Reliability Prediction has been received from the subcontractor and incorporated in this report. This prediction shows a significant increase of approximately 31 o/o due to incorporation of design changes.

Conclusions and Recommendations Discussion

This Mathematical Model Block Diagram and Prediction represents the second update of the interim ALSEP Program Phase II Prediction. This prediction is a further refinement of previous predictions for several reasons:

(1) The design is further defined and substantially firmed (2) ATM-501A "Failure Modes, Effects and Criticality

Analysis", dated 1 January, 1967 made possible the use of failure modes, effects and probability of occurrence to the piece part level.

5 4 ~ 3 2 1 RELIABILITY R E V I S I 0 N S CONFIG MGT

APPO PREDICTION ZONE LTR DESCRIPTION DATE APPV'D

0 I

l'f D Senaor D Central

Electronics Electro- I Station Mechanical ___;... Electronics ~ I-- 1-

c

PSO 1- •(0000) PSOZ--(0000) PSOl·-(00~

~

B I

QTY DESCRIPTION CODE PART OR ITEM REQD I DENT SPECIFICATION NO. PROPRIETARY NOTICE

!\

LIST OF MATERIALS THIS DRAWING CONTAINS UNLESS OTHERWISE SPECIFIED: CONTR NO. ( -B ~· ~] Systems Division INFORMATION PROPRIETARY DIMENSIONS ARE IN INCHES RAWN THE

TO THE BENDIX CORPORATION TOLERANCES CHECKED c ..... .rTIOH Ann Arbor, Michigan AND/OR ITS VENDORS AND DECIMAL ANGLES STRESS!WT TITLE PASS IV E.' SE:/SMOMETER SUPPLIERS. THIS DRAWING .X ± ± DSGN SUPV MAY NOT BE DISCLOSED TO .XX ± PROJ ENGR ~ELlA B/L ITY BL.oc K .I>IIH~ R!IM OTHERS FOR ANY PURPOSE PART NO. NEXT ASSY END ITEM NO. SERIAL NO. .XXX ± CHAMFER ±5° QUAL CONT NOR USED FOR MANUFACTURING DRAWING AND PART APPLICATION FINISH MICROINCHES RHR SYS SPT SIZE CODE !DENT NO. I DRAWING NUMBER PURPOSES WITHOUT THE

FINISH MATERIAL: SGN APPL B 07038 Ps o o WRITTEN PERMISSION OF THE DRAWING CLASS MFG BENDIX CORPORATION. AD s D cO CUSTOMFR SCALE LEVEL+ !WE I GHT sHEETA 3 7 or ,AI./ FORM NO. BS~3.tZA • KaE 10 SISS 10-66•

5 4 • 3 2 1 RELIABILITY R E V I S I 0 N S CONFIG MGT

APPD PREDICTION ZONE LTR DESCRIPTION DATE APPV'D

c

Elec. Calibration Short Power Power Assembly Attenuator Period Converter Converter

Elec. 1- "Art t-· "B"

PSO 1- -(I 000) PSO 1--(2000) PSOl--(3000) PSOl--(4000) PSOl--(5000)

c Level Switch Level Switch Long Period Long Period Long Period & Trig. Gen. & Trig. Gen. Elec. Elec. Elec. "YII

~~x" "Z 11 Axis 11 Y" Axis 11 X 11 Axis

PS01--(9100) PS01--LQOOOI PSOl-·(8000) PSO 1--170001 PSOl--(6000) ~

Level Switch Diptal Elec. Di&ital Elec. Digital Elec. & Tri&. Gen. Module Ill Module 112 Module 113 AID

"Z" Converter

PSOl·-(9200) PSO 1··(9300) PSOl--(9400) PSO 1--(9500) PSOl--(9600) B

QTY DESCRIPTION CODE PART OR ITEM

PROPRIETARY NOTICE REQD I DENT SPECIFICATION NO. LIST OF MATERIALS

THIS DRAWING CONTAINS UNLESS OTHERWISE SPECIFIED: CONTR ND. [..., .. ~1 Systems Division INFORMATION PROPRIETARY DIMENSIONS ARE IN INCHES DRAWN THE

TO THE BENDIX CORPORATION TOLERANCES CHECKED co.,our••• Ann Arbor, Michigan AND/OR ITS VENDORS AND DECIMAL ANGLES STRESS/WT TITLE C.E/1/~~L STATION ~L.ECiftO~ICS SUPPll ERS. THIS DRAWING .X ± ± DSGN SUPV REl.JAStL.17"f 8LOC!o'( OtA4iRIIM MAY NOT BE DISCLOSED TO .XX ± PROJ ENGR OTHERS FOR ANY PURPOSE PART NO. NEXT ASSY END ITEM NO. SERIAL NO. .XXX ± CHAMFER ±5° QUAL CDNT PASS IV£ SEf3Mo~ETE~ NOR USED FOR MANUFACTURING DRAWING AND PART APPLICATION FINISH MICROINCHES RHR SYS SPT SIZE CODE IDENT NO. 'DRAWING NUMBER PURPOSES WITHOUT THE

FINISH MATERIAL: DSGN APPL B 07038 PS Cl WRITTEN PERMISSION OF THE DRAWING CLASS MFG BENDIX CORPORATION. AD eO cO CUSTOMER SCALEt.&:V£L£1WE I GHT SHEET A 3 E'" oF At. I

A

FORM NO. BS-342A • KS:E 10!51155 1G-66•

5 4 • 3 2 1 RELIABILITY R E V I S I 0 N S CONFIG MGT

APPO PREDICTION ZONE LTR DESCRIPTION DATE APPV'D

) [

Sen• or Sensor Elec. Long Short Period Electronics "W" Board Period Calibration - X, Y, & Z - Preamplifier As,.embly

~ Axis

PSOZ--(1000) PSOZ--(2000) PSOZ--(3000) PSOZ--(4000)

I

' (

Long Period Long Long Calibration Period Period Uncage

• I...-. X, Y, & Z Axis 1------ Preamplifier Preamplifier Circuit 1---- .. PSOZ--(5000) PSOZ•-(6000) PS02-·(700Q] PSOZ·-{8000)

~ B

QTY DESCRIPTION CODE PART OR ITEM - PROPRIETARY NOTICE

REQD I DENT SPECIFICATION NO. LIST OF MATERIALS

THIS DRAWING CONTAINS UNLESS OTHERWISE SPECIFIED: CONTR NO. (...., -"·~} Systems Division INFORMATION PROPRIETARY DIMENSIONS ARE IN INCHES RAWN THE

TO THE BENDIX CORPORATION TOLERANCES CHECKED ;;:.,o;?roo• Ann Arbor, Michigan AND/OR ITS VENDORS AND DECIMAL ANGLES STRESS/WT TITLES ENSOR E t.Ec:TRoNJCS SUPPLIERS. THIS DRAWING .x ± ± DSGN SUPV #fEliASI&..tTY 8 t..cct( DIAGiRAM MAY NOT BE DISCLOSED TO .XX :1: PROJ ENGR 1 OTHERS FOR ANY PURPOSE PART NO. NEXT ASSY END ITEM NO. SERIAL NO. .XXX ± CHAMFER ±5° QUAL CONT PI1SSf\tE. S'EISMO METER NOR USED FOR MANUFACTURING DRAWING AND PART APPLICATION FINISH MICROINCHES RHR SYS SPT SIZE CODE IDENT NO. 'DRAWING NUMBER PURPOSES WITHOUT THE

FINISH MATERIAL: DSGN APPL B 07038 PS 0 d-. WRITTEN PERMISSION OF THE DRAWING CLASS MFG , BE~X COR_PORATION. AD B D co CUSTOMER SCAL~~L S~IWEIGHT SHEET A"3Cf CF /1[./

jj

FORM NO. BS-342A • K&E to 5Uil5 lo.G6•

)

.. ..

•

s

5

Long Period Hor. Boom Assembly (2)

PS03--(iOOO)

Leveling Stoo'

PS03--{9l 00)

Thermlll Control .___ __ Assembly

PS03-·(9200)

PROPRIETARY NOTICE

THIS DRAWING CONTAINS INFORMATION PROPRIETARY TO THE BENDIX CORPORATION AND/OR ITS VENDORS AND SUPPLIERS. THIS DRAWING

~ MAY NOT BE DISCLOSED TO OTHERS FOR ANY PURPOSE PART NO. NOR USED FOR MANUFACTURING PURPOSES WITHOUT THE

4

Spring G•ging Assembly -

PS03--(2000)

Leveling Drive ·-----·--Assembly (2)

PS03·-(9000)

Sensor Assembly

PS03--(9300)

NEXT ASSY END ITEM NO. SERIAL NO. DRAWING AND PART APPLICATION

WRITTEN PERMISSION OF THE DRAWING CLASS FINISH BENDIX CORPORATION. AD BDcD FORM NO. BS-342A

• 3 2 1 RELIABILITY R E V I S I 0 N S CONFIG MGT

APPD PREOI CTI ON ZONE LTR DESCRIPTION DATE APPV'D

Mass Gaging Gimb•lled Upper Bellows Platform Platform

Assembly (3) Assembly Assembly

PS03--(3000) PS03--(4000) PS03--(5000)

(

Uncaging Base Mech. Assy. Enclosure Bctam ---·--- Assembly ··-.. ·-··-

Assembly

PS03--(8000) --p-so3--(7000) PS03--(o000) ...

Bubble Mercury Short

Level Switch As•y • Period Vertical Assemblv

PS03--(9400) PSO'--to<;oO\ PS03- -(9600) E

QTY DESCRIPTION CODE PART OR ITEM REQO I DENT SPECIFICATION NO.

LIST OF MATERIALS UNLESS OTHERWISE SPECIFIED: CONTR NO. [...., .. ~l Systems Division

DIMENSIONS ARE IN INCHES RAWN THE

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