232-11704.pdf

APPLICATION

PART NUMBER NEXT ASSY USED ON EFFECTIVITY

AGM-86'

FOR REVISION DESCRIPTION SEE REVISION SHEET.

NOTES ARE SHOWN IN SECTION 6.

Statement D, DOD and US DOD Contractors only, OC-ALC/ENSDAA 3001 Staff Drive, Suite 1AB82A

Tinker AFB, OK 73145-3041

"WARNING- EXPORT CONTROLLED"

[0 FOR THE TOTAL NUMBER AND REVISION STATUS OF SHEETS, SEE ACTIVE SHEET RECORD

CONTROLLED INTERCHANGEABLE PART

232-11704-( ) I

ENVELOPE DRAWING

: ��;f�l1i�iEs

CONTR Fz:3{.J;"51 _:·�·2-t..,i-�:,l.;, THE BOEING COMP AN'(

REY

....,_ EX·:EPTAS DR

NO fED ______ ........ ......__........_.,...._._,_"-+-__ CORPORATE OFFICES SEATTLE, WASHINGTON 98124 CHK ti/ t o

;-,---•------------........ -------4

'-,l ----t· / 1,i--,-,/ \:; �- DWG ORIG BY

2--6052 E '¼.

CHAI-, GE NO.

TCP 121--

SERVO ASSEMBLY,FLIGHT CONTROL

CODE IDENT NO.

81205

SCALE REV

232-11704

SHEET

SHEET _,

NO. >

w ""

1 q

2 {,--}

3 g

4 A

5 C

6 C

7 C

8 A

9 C

10 D

11 F

12 C

13 -

14 D

15 F t G

17 D

18 C

19 F

20 C

21 F

22 A

23 C

24 C

25 -

26 -

27 C

28 C

I 29 F

30 F

31 C

32 E

33 B

34 D

35 C

36 D

37 C

38 D

39 C

40 C

41 A

42 A

43 -

44 - 45 -

SHEET

NO.

4.1

4.2

4.3

4.4

4.5

4.6 10.1

11.1

12.1

20.1

29.1

34.1

38.1

ADDEO

I

I-w °'

A

A

A

A

A

B i;.,.+ F E

C

C

C

C

ACTIVE

SHEETS

SHEET

NO.

4.7

4 .. 8

4.9

4 .10 4.11

4 .12 4.13

11.2

12. 2

I I

SIZE"

A

SCALt:

SHEET RECORD

...J w ""

C

C

C

D

F

F

H

SHEET

NO.

CODS IDE::NT NO.

81205

IREV

I- ...I w ""

A

B

F

F

C

F

F

B

D

C

C

A

E

E

E A

C

C

C

C

A

C C

B

C B

C

C

C

C

C

C

L_ -��- ·---·-" ------ - ':.'l 4(10� !··04('. t"\EV {.,/7�

I

ADDED SHEETS

SHEET ...J SHEET �

NO. > NO. >

UJ w ""' ""

57.1 D

61.1 A

64.1 C

66.1 A

86.1 C

232-11704

I

Ii ISHtH 2

J15-047

ACTIVE SHEET RECORD •

ADDEO SHEETS ADD ED SHEETS

SHEET -' SHEET

SHEET -' SHEET -' SHEET -' SHEET ...

NO, > NO. > NO. > NO. > NO. > NO. >

w w

"" "" w UJ w "' o, ""

91 C

92 A

93 -

94 -

95 -

96 -

97 -

98 A

99 A

100 D

101 E

102 C

103 C

104 E 104 .1 C

105 -

106 C

107 C

108 C

109 C

110 C

111 .. F 112 F 112 .1 F.

113 D 112.2 C

114 D 112. 3 C

115 C 112 .4 C

112. 5 C

112 .6 F

117 I I

,-:-5

I i I . �

SIZf' CODE IDrnT NO.

J A 81205 232-11704

L-•=-·ca·=•-•�--.. -·-�

SCALE IREV � I SHEET 3

:- , -150\ t1b40 PE'v t/73 J15-047

REVISION

LTR l 01:SCRIPTION

A I

D232-10554-1 Release under Contract No. F33657-77-C-0226.

� Sht. 1 Added revision letter.

l

Sht. 2 Added revision letter and added sheet numbers.

Sht. 3 Added revision letter and added sheet numbers.

Sht. 4, Added revision description.

4.1, 4.2, 1 4.3, 4.4, l 4. 5

Sht. 8 Added "4. 1. 3. 5 .14 Fatigue Load 11

Sht. 10 Added -11 mockup assembly.

Sht. 11

I Sht. 12

Added -12 and -13 mockup units.

Added -11, -12 and -13 mockup assembly and units. l

Sht. 14

Sht. 15

Sht. 16

Revised issue of L-P-378D, QQ-P-416C, PPP-F-320D, MIL-B-5087B and MIL-C-38999F.

Deleted TT-E-527C and MIL-C-46842A.

Added PP-C-1752A.

Revised issue of MIL-C-83286B, MIL-E-6051D, MIL-F-7179E, MIL-F-14265D, MIL-I-8500C and

MIL-M-38510B.

Revised issue of MIL-P-116F, MIL-P-23377C, MIL-S-77428, MIL-S-8879A, MIL-S-19500E, MIL-S-81733A, MIL-T-83399.

Sht. 17 Revised issue of MIL-STD-129F, MIL-STD-130D, MIL-STD-198C, MS33750E, FED-STD-595A.

1 Sht. 18 Revised issue of MIL-STD-199B, MIL-STD-454D, , MIL-STD-462, MIL-STD-701J, MIL-STD-704A and MIL-STD-490.

i Sht. 19 Revised issue of MIL-STD-961 and MIL-STD- 1472B.

Sht . 20 Revised issue of MIL-HDBK-5, MIL-HDBK-23, MIL-HDBK-217B, ALCM Doc. 239 and

, MIL-HDBK-17A.

CODI: IDl:NT NO.

DAT!: APPROVAL

DRAWN:

Ct\ Ll lk/?J_ .. �;...1·;,. ,_ '

A. Harris

81205 232-11704

SCALI: I REV L

01 4315 8000 REV. 9/73 ... J15-047

LTR

A Sht. 20.1

Sht. 21

1 Sht. 22

Sht. 23

Sht. 24

Sht. 27

Sht. 28

Sht. 29

Sht. 30

Sht. 32

Sht. 33

Sht. 34

REVISION

DESCRIPTION

New sheet added for continuation.

Revised issue of D232-10337-1 (S), D232-10327-l, 232-11706 and 232-11707.

3.2.1.1: Added ref. to 3.2.1.8.

Figure 1: Added: 11 (to be provided by Supplier.)"

Figure 2: Changed note on JS to allow definition by supplier.

3.2.1.3.2: Changed +5mv to �9mv; define load impedance.

Figure 4: Removed boundaries in backdrive quadrants and words 11unacceptable.11

3.2.1.3.3.c: Defined load impedance.

3.2.1.3.4: Replaced with: "To be provided by Supplier. 11

3.2.1.3.5: Supplier to define test signals.

3.2.1.4.1.e: Redefined ripple currents.

3.2.1.5: Removed 11 Position" from title.

3.2.1.7.1: Deleted 11 • • • by locking armature, II

3.2.1.8: Defined impact energy.

3.2.1.9: Revised to reflect deflection against a positive spring.

Sht. 34.1 New sheet added for continuation.

Sht. 34.1 3.2.1.10: Added load definition to first paragraph.

Added unbalance load component to inertia in fourth paragraph.

CODE IDENT NO.

DATE

SIZt=

81205 232-11704

SCALE l SHEET

DI 4315 8000 REV, 9/73

APPROVAL

JlS-047

LTR [

A Sht. 38

Sht. 38.1

Sht. 39

Sht. 40

Sht. 41

Sht. 42

Sht. 47

Sht. 50

Sht. 51

Sht. 57

Sht. 61 c·

Dl 4315 8000 REV. 9/73

REVISION

DESCRIPTION I DATE I APPROVAL

3.2.1.12: Increased friction values.

3.2.1.13, 3.2.1.14 and 3.2.1.15: Replaced with: "To be provided by Supplier."

3.2.3.1: Added Controller and Actuator MTBF's.

3.2.3.2: Added Controller and Actuator MTBMA's.

New sheet added for continuation.

Figure 8: Deleted curve and added note, "To be provided by Supplier."

Figure 9: Deleted curve and added note:

"To be provided by Supplier."

3.2.3.5: Changed ... "fifteen {15) ... '' to " ... ten ( 10) .... "

3.2.5.1.2.c: Added parentheses.

Figure 11: Revi sect curve.

Added new section: "3.2.5.1.2.k.

Eatique load."

3.2.5.2.2.d: Deleted reference to ejector axis and missile centerline.

3.2.5.2.2.j: Changed .214 to .82.

3.2.5.2.2.l: Changed .214 to .82.

3.2.5.3: Specified recovery period after nuclear-induced upset.

3.3.1.3.6: Allowed lifting of voltage sensitive components.

3 . 3 . 8 . 1 : Ch an g e d " ... 2 0 0 ... " to " ... 3 O O ... " 3.3.8.1.1: Increased long term storage period. Added cycles and period of operation.

3.3.8.2: Allowed orientation in any direction during active employment.

3.3.8.7: Replaced with: "To be provided by Supplier."

SIZE CODE IDENT NO.

A 81205 232-11704

SCALE IREV A lsHEET

JlS-047

A Sht. 61. 1

Sht. 62 i

Sht. 64

I

REVISION

DE::SCRIPTION

New sheet added for continuation.

3.3.8.11: Changed " ... 320

F. 11 to " ... 430°F." and deleted modification to mission duty cycle.

3.3.8.13 and 3.3.8.14: Replaced with:

"To be provided by Supplier."

4.1.2: Deleted Stress Verification Measure ment.

4.1.2.1: PRVT required for CET units;

required controllers to be energized electrically during entire CET.

4.1.2.1.1: References to Table IV and Figure 14 removed.

DATE::

, Sht. 64. 1 New sheet added for con ti nuati on.

1 Sht. 65

Sht. 66

Sht. 66.1

Sht. 67

Sht. 70

Sht. 75

Sht. 83

Sht. 84

Dl 4315 8000 REV. 9/73

Figure 14: Removed operation during Steps 4 and 8; reduced soak time, Steps 2 and 6.

4.1.2.1.1: Step 2: Reduced soak period energize controller for entire CET; Step 4:

deleted operation; Step 5: revised chamber humidity; Step 6: reduced soak time; Step 7:

revised chamber humidity; Step 8: revised humidity; deleted operation.

New sheet added for continuation.

Table IV: Deleted "Humidity" column and revised Step 2 "ABS PRESS. II

4.1.2.2: Deleted.

Added item 3.2.5.1.2.k.

4.1.3.2.h: Added reference to 3.2.3.3.

4.1.3.4.6: Revised titles.

4.1.3.4.6.b: Added tolerance to stiffness value.

SIZE:: com= IDE::NT NO.

A 81205 232-11704

SCALE:: IREV

I SHE::[:T

/I . ..-,, ,.._..f" I•:·

J�5-047

LTR I

A Sht. 86

Sht. 87

Sht. 88

Sht. 89

Sht. 92

Sht. 98

Sht. 99

REVISION

DESCRIPTION

4.1.3.4.6.c: Revised spring value and added friction limit.

4.1.3.4.6.e: Deleted coulomb friction loads

4.1.3.4.6: Described inertia load for PRVT, CET, and Vibration Qualification Test.

4.1.3.5: PRVT required for Qualification !

Test units.

4.1.3.5.1: Operated according to complete I Mission Duty Cycle (3.2.1.9.1) and deleted coulomb friction load; changed " ... 320° F.11 to

• • • 430° F. 11

Table VII - Sht. 1: Added column

"FATIGUE LOAD"

Table VII - Sht. 2: Added column

II FA TI GUE LOAD"

Table VII - Sht. 3: Added column

11 FATIGUE LOAD"

4.1.3.5.9:

4.1.3,5.8:

Figure 17:

Revised shock duration to range.

Change J'"P-9" to 11 JP-4," Revised curve.

Figure 18: Revised curve.

Sht. 100 Added: "4.1.3.5.14 Fatigue loads."

Sht. 101 4.1.3.6.1, 4.1.3.6.5, 4.1.3.6.6 and 4.1.3.6.7: Replaced with "To be provided by Supplier."

Sht. 103 4.1.3.6.12: Changed velocity at stop impact to supply voltage and removal of one 15 VDC supply.

4.1.3.5.13: Commanded constant deflection plus position square wave plus triangular wave with spring-damper-inertia and external spring loads.

Sht. 107 4.2.2.1.f: Replaced with: "To be provided by Supplier."

SIZE COD!= IDrnT NO.

A 81205 232-11704

DATE I APPROVAL

I

I

SCALE IREV I-\ I SHE:-E:-T (

Dl 4315 8000 REV, 9/73 ... J t 5-047

LTR I

A Sht. 109

Sht. 110

Sht. 111

Sht. 112

REVISION

DESCRIPTION

4.2.2.1.k and 4.2.2.1. l: Replaced with:

"To be provided by Supplier."

4.2.2.1.o, 4.2.2.1.p and 4.2.2.1.q:

Replaced with "To be provided by Supplier."

4.2.2.1.v: Replaced with: "To be determined. :

4.2.3: Deleted Actuator PRVT; reduced 15 temperature cycles to 10 temperature cycles; required operation during each temperature cycle; PRVT is prerequisite for CET and Qualification Test units.

Table VII: Removed middle 5-cycle block;

initial random vibration and acceptance tests are optional; redefined "RELIABILITY

DEMONSTRATION. II

I Sht. 115 6.2: Added 11 [I> 11

Reason for change: Basic release to incorporate technical baseline.

SIZt= COD� IDrnT NO.

DATt=

A 81205 232-11704

SCALt: IREV i\ jsen=u

01 4315 B000 REV. 9/73

APPROVAL

J\5-D47

B PRR 9501

ADCN

NUMBER

D1 431� 8000 REV. 9/73

REVISION

DESCRIPTION

I nco r�o rates ADCN'S 1 through 16

SEQUENCE

NUMBER

IA

2A

9A (Cancelled by 15)

3A lOA

7A

SA

4A

BA

6A llA

12A

16A

13A

14A

15A

SIZE

SCALE

CHANGE

NUMBER

PRR 9500

PRR 9500

PRR 390

PRR 9500

PRR 390

PRR 9500

PRR 9500

PRR 9500

PRR 9500

PRR 369

PRR 390

PRR 390

PRR 9500

PRR 435

PRR 390

PRR 390

CODE !DEN • NO.

81205

REV B

DATE

9��\�'lt

• f If 'I ,·' ' I I I, ! .-

·1�7(:, J1-t•'"I

·I

232-11704

APPROVAL

cJ . I l,.J,J.. /l-''4,' 9 2o Y

WLWriglit

'// IL /. , I •

.' c..,.;_ I .. , ,, Li, (

;a:.

.H. Chase f PEGrafton

�I• f' Ir _,L

MDMob l ey ,_·, SHEET 4. 6

J\5-047 r

C

Dl:c5CPIPT!ON

PRR 9501 Incorporates ADCN's 17 through 60

ADCN

NUMBER

SEQUENCE

NUMBER

12B 13B 14B 15B 16B 17B 1B

18B

19B 2B 3B 4B* 5B 6B 7B 8B 9B lOB 20B 21B

22B llB

CHANGE

NUMBER

PRR 9500

j

PRR 9500

PRR 518

PRR 518

PRR 492

PRR 492

PRR 9500

PRR 9500

PRR 9500

PRR 560

ADCN

NUMBER

SEQUENCE CHANGE

NUMBER NUMBER

23B 24B 25B 26B 27B 28B 29B 30B 31B 32B 33B 34B 35B 36B 37B 38B 39B 40B 42B 43B 44B

PRR 9500

PRR 9500 .

I

PRR 9500

*Replaced

PRR 9500

by ADCN 35.

Sht. 27

Sht. 59

Sht. 73

Sht. 87

Paragraph 3.2.1.3,J, first paragraph - changed "position 11 to 11positive. 11

Retyped. Revised Paragraph 3.3.2.5, fourth paragraph to add 11 Transient pulses which occur during 28 voe and/or + 15 voe power turn-on are exempt from this requirement. 11

Revised Paragraph 3.3.3 a to add -26 unit.

Revised Paragraph 3.3.3 b to add -18, -19, -21, -28 and -29 units.

Table VI, Paragraph 3.2.1.16 - manged "Gain Margin" to 11L imit Cycle."

Table VII, Paragraph 3.2.1.16 - Changed "Gain Margin" to "Limit Cycle. 11

DATE APPROVAL

(C)DC IDrnT NO

81205 232-11704

SCALE I REV C !sHt:U 4.7 Dt 4315 8000 REV. 9/73 .... J 15-047

Ui, C PRR 480

Sht. 1 Sht. 2, 3 Sht. 4.7, 4.8,4.9

Sht. 11. 1 Sht. 12 Sht. 14 Sht. 15

Sht. 16

Sht. 17

Sht. 18

Sht. 19

Sht. 20

Sht. 20.1

Sht. 21

Sht. 51

Sht. 52

Sht. 54 Sht. 55

Sht. 57

Sht. 57.1

Sht. 76

01 43�5 8000 REV, �/73

REVISION

Dfc.SCRIPTION

Added Revision letter.

Update Active Sheet Record.

Added Revision C description.

Added -19 actuator.

Added -19 actuator.

Changed issue date of MIL-C-8956 (1).

Added Appendix A to MIL-E-8189H and Note*.

Changed date of MIL-M-38510C.

Retyped. Added MIL-P�28809, MIL-P-55110B (2), MIL-P-55640A (2), MIL-S-45743C, MIL-W-5088F, and Note*. Changed issue date of MIL-T-83399.

Changed issue date of MS-21244A and added Notice 2 of MIL-STD-129F.

Retyped. Added MIL-STD-275C and changed issue date of MIL-STD-461A.

Retyped. Added MIL-STD-1495 and Note*.

Changed issue date of MIL-STD-961 and

AFR 73-1.

Changed date of AFSC DH 1-3, MIL-HDBK-5, MIL-HDBK-23A, and MIL-HDBK-217B.

Changed date of ALCM Document 239B and

MIL-BUL-147.

Retyped. Added D232-10337-3, 232-11299, Note*, and Note**.

Retyped. Added Paragraph 3.2.5.3.1, Production Hardness Assurance.

Retyped. Revised Paragraph 3.3 to add second sentence "In addition ..... modification. 11

Moved Paragraph 3.3.1.1.2 from sheet 55.

Retyped. Moved Paragraph 3.3.1.1.2 to sheet 54. Revised Paragraph 3.3.1.1.2 i soldering requirements.

Retyped. Added Paragraph 3.3.1.3.4.1 and 3.3.1.3.4.2.

Added sheet for Paragraph 3.3.1.3.6 and

3.3.1.4 a previously on sheet 57. Added Paragraph 3.3.1.3.7.

Table VI - added "3.2.5.3.1. ... Production Hardness Assurance .... 4.2.4."

coo= IDrnT NO.

DATE

81205 232-11704

SCALE I REV C jsHEET 4.8

J\5 047

LT le

C

Rl:V ISION

Di=SCRIPTION

PRR 480 (Continued)

Sht. 111 Retyped. Changed PRVT requirements for -2 and -18 units, Paragraphs 4.2.3.2 through

4.2.3.2.2.2. Moved Paragraph 4.2.2.1 s, t, Sht. 112 .2 Sht. 112 .3 Sht. 112 .4

Sht. 112. 5 Sht. 112. 6

Sht. 116

PRR 492

Sht. 10 Sht. 11.1

Sht. 12.1

Sht. 27

Sht. 29

Sht. 30

Sht. 31

Sht. 115 u, and v to sheets 109 and 110.

Added Figure 20.

Added Figure 21.

Changed PRVT requirements for -2 and -18 units, Paragraph 4.2.3.2.2.2 a through 4.2.3.2.4.1.

Added Figure 22.

Changed PRVT requirements for -2 and -18 units, Paragraph 4.2.3.2.4.2 and 4.2.3.2.5.

Added Hardness Assurance Paragraph 4.2.4.

Added Military Specification Paragraph

4.2.5 through 4.2.5.1.3.

Revised Note ill> and [[> .

Added -25 Engineering Model.

Added sheet for overflow from sheet 11.

Added -26 Engineering Model Controller.

Added sheet for overflow from sheet 12 Added -25 and -26 Engineering Model units.

Paragraph 3.2.1.3.2, first paragraph, last sentence - Changed 11TB0 11 to 11100 11 millivolts.

Retyped. Paragraph 3.2.1.3.2.1, second sentence - Changed 11TB0 11 to ".050" voe and added "at actuator mechanical null (0 degree). 11

Retyped. Paragraph 3.2.1.3.6 - Added 7 + ".110" voe and 11 + ".140" voe tolerance. Moved Paragraph 3.2.1.4.1 a, b, c, d, and e to sheet 31.

Retyped. Moved Paragraph 3.2.1.4.1 a, b, c, d, and e from sheet 30.

Retyped. Added -25 and functional description to Note tI>.

SIZb CODi= IDl'fH flO.

DATE

A 81205 232-11704

SCALi= REY C

'01 4315 8000 REV. 9/73

APPROVAL

f.O. .'U/4._.._

R.A.URBAN

4.9 Jl5-0.47

Rl:V ISION

Db-.SCRIPTION

D PRR 9501 Incorporates ADCN's 61 through 68

ADCN SEQUENCE CHANGE

NUMBER NUMBER NUMBER

61 lC PRR 577

62 2C PRR 9500

63 4C PRR 9500

64 6C PRR 9500

65 7C PRR 9500

66 SC PRR 9500

67 SC PRR 9500

68 3C PRR 628

COD:C IDE::NT NO.

A 81205

SC: ALE REV

"Dl 43!5 8000 REV. 9/73

D

DAE APPROVAL

G --/- - - +-,-,-,c--,-"�,,,,'c-;�..,..--c------t MDMobley

2 32-11704

SHE eel

G 11 , i i ' I c:1-

4.10

J15-047

E

REVISION

Di=SCRIPTION

PRR 9501 Incorporates ADCN 1 s 69 through 96

ADCN SEOUENCE CHANGE

NUMBER NUMBER NUMBER

69 1D

70 20 71 3D 72 4D 73 50

74 6D

75 7D

76 (CANCELLED BY ADCN 81) 8D

77 (CANCELLED BY A0CM 82) 90

78 (CA !CELLED BY !">.0CN 90) 10D

79 (CANCELLED BY A0CN 92) 11D

81 ( r.ANCFLLEn BY ADCN 88) 120

82 (CMCELLED BY ADCN 89) 13D

83 (CANCELLED BY ADOI 91) 14D

84 (CMICELLED BY ADCN 92) 15D

00 1@ 85 17D

� 100

88 (REPLACED BY ADCN 93)

89 (REPLACED BY A0CN 94)

91 (R r "'L" "E,..., n" "DC•' g c)C. t' /-'I l, U D 1 f-1 I� ;J

92 (REPLACED BY ADCN 96)

93-

19D 20D

LLU

25D 28D

D232-10916 D232-10916

PRR 695

PRR 9500

PRR 9500

PRR 9500

PRR 9500

PRR 777

PRR 777

PRR 777

PRR 777

PRR 784

PRR 784

PRR 784

PRR 784

PRR 9500

PRR 9500

PRR 9500

ECP 802

PRR 802

PRR 802

PRR 802

PRR 802

PRR 408

PRR 9500

PRR 9500

PRR 9500

PRR 9500

DATE APPROVAL

s/14l�l �.O.� RAUrban

5/s/21 i?.D.� RDTucker

\h:k0; / l MDMobley

1 l '

* These ADCN 1 s include the intent of PRR 777, PRR 784 j and PRR 802 which was included in ADCN 1 s 76-79, l

81-84, 88-89, 97 and 92.

w_�-_-12-c·�-,;�-�--�-�;�:'.�-�;0-4--� __ -.�---_j j :'._,,__ � J,�- F _l_'. 'LY _ 4.11 _ '

.: I: - ·:,�?

I

REVISION

LTR DESCRIPTION DATE APPROVAL

F PRR 9501 - INCORPORATED THE FOLLOWING ADCN'S: iz;e (g3 ( -:• o/.,, ADCN NO. SEQUENCE CHG. NO. L.A. Bo_yer

12.li\i-:, <;20.:' 97 lE PRR 9500

;-;� 98 2E PRR 9500 ,l.-( 'ti �l99 3E (REPLACED BY ADCN 114) PRR 827 G. V.Oswald 100 4E PRR 827 'f' --S�l!

/'/� �-.I {ct_ 101 5E PRR 827 )S R. D. Craig 102 6E (CANCELLED BY ADCN 103) PRR 827 1ft; 3 -_ l!�103 7E PRR 9500 y

104 SE PRR 9501

0 j/ --P

\-'""1

105 9E PRR 9500 1/<'f:;d-- , +/'Y!.•-�,, .. < _, ; 1 S. J. Fount 106 lOE ECP 349

��,,? n}�· ..._ "' �c

107 llE PRR 9500 , q3 C. Charlton

108 12E (REPLACED BY ADCN 115) ECP 492

109 13E (CANCELLED BY ADCN 112) ECP 492 \· I

110 14E (CANCELLED BY ADCN 113) ECP 492

"I

I

111 15E (REPLACED BY ADCN 116) ECP 500

·112 HiE ECP 500

113 17E ECP 500

114 18E PRR 9500

115 19E PRR 9500

116 20E PRR 9500

117 21E PRR 9500

118 22E PRR 9500

119 23E PRR 9500

120 24E PRR 9500

CODc: !DENT NO.

A 81205 232-11704

SCALE REV F 4.12

U1 �315 BODO REV. Q/73 Jl5-047

REV

G

H

REVISIONS

DESCRIPTION

PRR 9501 - Incorporated the following AOCN's:

ADCN NO.

SEQ NO. CHG NO.

lF (Cancelled by AOCN 122) PRR 9500

122 2F PRR 9500

MFG ENGR: {1.� frC. -€-19

QA ENGR: .led;� c--'1-f,-10

ECP 198

Reason: Vendor Part Number is changing for refurbishment with an improved lubricant. Contract FA8119-08-C-0024 "Sustainment Engineering and Support Technical Inquires for Business Unit as ALCM/CALCM".

Sh.

1, 2 4.13 10.1 11.2 12.2

Description Revised.

Added Revision H description.

Added new Servo Assembly configuration -46.

Added new Actuator configuration -47.

Added new configurations -46 and -47.

Revised para 3.3.3.b for -47 configuration.

Added Flagnote 20.

10/05/04 '��-� H. Fromm 01/05/04

D. Peace 10/05/04

B. Maritvold a::1t\-C,'J-<.):.f

CAGE 81205 SIZEA DWG NO. 232-11704 SH 4.13 REVH

z w V, l 1.1 l.2

3. l

3. l . l

3. l. 2

3. l . 2. l

3. l . 2. 2

3. l.3

3. l .4

3. l. 5 3.2

3. 2. l 3.2.1.l

3. 2. l . 2 3.2.1.2.l 3.2.1.2.2

3. 2. l . 3 3.2.l.3.l 3.2.1.3.2 3.2.1.3.2.l 3.2.1.3.3 3.2.1.3.4 3.2.1.3.5

3.2. l .3.6 3.2.1.4

3.2. 1.4. l 3.2.l.4.2 3.2.1.4.3 3.2.1.5

3. 2. l. 6 3.2.1.7 3.2.l.7.l

3.2.1. 7 .2

3.2.l.7.3

3. 2. l . 8

3. 2. l. 9 3.2.l.9.l

3.2. l .9.2 3.2.1.10 3.2.l.ll 3.2.1.12 3.2.1.13 3.2.1.14 3.2.l.15 3.2.1.16

DI 4316 2000 REV. 4/73

TABLE OF CONTENTS

SCOPE

Scope Classification

APPLICABLE DOCUMENTS

REQUIREMENTS

Item definition Functional interface diagram Interface definition Physical interface Electrical interface Major components Government furnished property list Government loaned property list Characteristics Performance Angular displacement Angular velocity versus torque Backdrive Dynamic loading Interface signal characteristics Input command signal characteristics Position monitor signal characteristics Electrical/mechanical offset Motor current monitor signal characteristics Controller-actuator power Test signals Controller reference voltage output Power supply characteristics 28 VDC electrical power supply characteristics ±15 VDC electrical power supply characteristics Low voltage operation Position accuracy and resolution Backlash Stiffness Locked rotor stiffness Functional stiffness Dynamic stiffness Overtravel stops Duty cycle Mission duty cycle Ground checkout duty cycle Frequency response Acceleration Friction Torque gain Back EMF Threshold voltage Limit cycle

SIZE

A

Jl�47 z

-<i o,;

UJ

UJ

V')

3.2.2 3.2.3

3. 2. 3. l 3.2.3.2 3.2.3.3 3.2.3.4 3.2.3.4.l 3.2.3.4.2 3.2.3.5 3.2.3.6 3.2.4

3. 2 .4. l 3.2.4.2 3.2.5 3.2.5.l 3.2.5.l.l

3.2.5. l .2 3.2.5.2 3.2.5.2.l 3.2.5.2.2 3.2.5.3 3.2.5.3.l 3.2.5.4 3.3

3. 3. l

3.3. l. l 3.3.l.l.l 3.3.1.l.2

3.3. l. l.3

3.3. l. l.3. l 3.3.1.1.3.2 3.3.l.2 3.3.1.2.l 3.3.1.2.l.l 3.3.1.2.1.2 3.3.1.2.l.3 3.3.l.2.l.4 3.3.1.2.l.5 3.3.l.2.l.6 3.3.1.2.l.7 3.3.1.3 3.3.1.3.l

3.3. l .3.2 3.3.1.3.3 3.3.1.3.4 3.3.l.3.4.l 3.3.1.3.4.2 3.3.1.3.5

01 4316 2000 REV. 4/73

TABLE OF CONTENTS (CONTINUED)

Physical characteristics: weight and size Re 1 i ab i 1 ity Flight mean time between failure (MTBF) Meantime between maintenance action (MTBMA) Stress verification Combined environment Combined environment operation Combined environment failure Product reliability verification Aging Mai nta i nabi 1 ity Test provisions Repair and access Environmental conditions Non-operating environment Natural environment Induced environment Operating environment Natural environment Induced environment Survivability/vulnerability Production hardness assurance Storage Design and construction Materials, processes and parts Materials and processes Materials allowable Corrosion prevention/control Moisture and fungus resistance Fungus resistance Moisture resistance Standard, commercial and qualified parts Fasteners Design standards Screwthreads Screw recesses Spline drives High temperature clamps Self-retaining bolts Fatigue-rated fasteners Electrical Installation Selection of electrical/electronic parts Non-standard part specification Packaging Printed wiring boards and assemblies Metal core printed wiring boards Insulation resistance

CODE iDENT. NO.

.}15-,0,17

UJ

V')

3.3.1.3.6

3.3.1.3.7

3.3.1.4 3.3.2 3.3.2.1 3.3.2.2 3.3.2.3 3.3.2.4 3.3.2.5 3.3.3 3.3.4 3.3,5 3.3.6 3.3.6.1 3.3.6.1.1 3.3.6.2 3.3.6.3 3.3.6.4 3.3.7 3.3.8 3.3.8.1 3.3.8.1.1 3.3.8.1.2 3.3.8.2 3.3.8.3 3.3.8.4 3.3.8.5 3.3.8.6 3,3.8.7 3.3.8.8 3.3.8.9 3.3.8.10 3.3.8.ll 3.3.8.12 3.3.8.13 3.3.8.14 3.4 3,5

3.5 .1 3.6 l� 4.1 4.1.1 4.1.2 4.1.2.1

Dl 4316 2000 REV. 4/73

TABLE OF CONTENTS (CONTINUED)

Dielectric strength Wiring Reliability design requirements Electromagnetic radiation Electromagnetic compattbili ty E-field environment Bonding Power and signal return isolation Offset voltage Nameplates and product marking Workmanship Interchangeability Safety Electrical safety Connector contact assi.grunents Personnel safety Explosive safety Factors of safety Human engineering Design Operational service life Useful life Utilization rate Seals Deleted Lubrication Rod end bearings Castings Potentiometer Anti-rotation Drive motor type Null adjustment Heating effect Thermal control Impedance Inertia Documentation T,ngi !"ir.i f!S

Maintenance Precedence

QUALITY ASSURANCE PROVISIONS

General Engineering test and evaluation

Deleted CET test

SIZE CODE IDENT. NO.

A 81205

SCALE lREY

232-11704

C 1 SHE ET t

.J 1!',.,(1.47

-1

.,j z u., "'

I I

4.1.2.1.1 4.1.2.2 4.1.3 4.l.3.1 4.1.3.2 4.1.3.3 4 .l. 3.4 4.1.3.4.1 4.1.3.l+.2 4.1.3.4.3 4.1.3.4.4

4.1.3. !1.5 4.1.3.4.6 4.1.3.5 4.1.3.5.1 4.1.3.5.2 4.1.3.5.3

4.1.3.5. l� 4.1.3.5.5 4.1.3.5.6 4.1.3.5.7 4.1.3.5.8 4.1.3.5.9

4.1. 3. 5 .10 4 .1.3.5 .11 4 .1.3. 5 .12 4.1.3.5.13

4. l. 3. 5 .14

4.1. 3.6 4.1.3.6.l 4.1.3.6.2 4.1.3.6.3 4.1.3.6.4 4.1.3.6.5 4.1.3.6.6 4.1.3.6.7 4.1.3.6.8 4.1.3.6.9 4.1.3.6.10

4.1. 3.6.ll 4.1.3.6.12 4.1.3.6.13 4.1.3.6.14

4.1. 3 .6.15 4.1.3.6.16 4.1.3.6.17

4.1. 3.6.18 4.1.3.6.19

U'-\SE ='-"""" ___

Dl 4315 2000 �EV. 4/73

TABLE OF OONTE

N

TS (CONTINUED)

Test method Stress verification measurement Qualification Inspections Analyses Qualification test Test criteria, test equipment, and conditions Responsibility for tests Satisfactory operation and failure criteria Test equipment Calibration Instrumentation Load test fixture Environment tests High temperature Low temperature Temperature-hwnidity-altitude Dust (fine sand) Fungus Salt fog Acceleration Explosive atmosphere Shock Vibration Acoust.ic Low pressure Survivability/Vulnerability Fatigue load Performance design tests Controller actuator power Position accuracy and resolution Frequency response Friction Torque gain Back EMF Threshold voltage Low supply voltage Stiffness-locked rotor Stiffness-functional Stiffness-dynamic Overtravel stops Mission duty cycle Ground check duty cycle Heating effect Electromagnetic compatibility Bonding Signal/power returns E-field environment

SIZE CODE IDENT. NO. 232-]]704

A 81205

IR.:.v � I SHEET 1:CALE

B

.J ��·7

4.1.3.6.20

4.1.3.6.21

4.1.3.6.22

4.1.3.6.23

4.1.3.6.24

4. 1. 3. 6. 25

4.1.3.6 .26

4.1. 3.6.27

4.1 .3.6.28

4.2

4. 2. l

4.2.2

4.2.3

4.2.4

4.2.5

5. 1

5.2 >- 5.3

5. 3. l

5.3.l.l

5.3.l.2

5.3.l.2.l

5.3.l.2.2 z

5.3.1.2.3

5. 3. l. 3

5.3.1.3.l

5.3.1.3.2

5.3.l.3.3

5.3.2...

w 5.3.2.l

5.3.2.2

5.3.3

DI 4315 2000 REV. 4/73

TABLE OF CONTENTS (CONTINUED)

Signal/Power offset voltage Factors of safety Dynamic loading Operational service life Limit cycle Angular velocity vs torque Backdrive Acee 1 era tion Inertia Quality conformance inspection Inspection Acceptance tests Product reliability verification test (PRVT) Hardness assurance compliance Military specifications

PREPARATION FOR DELIVERY

General Specific requirements Detailed preparation Preservation and packaging Cleaning and drying Level A Wrapping material Cushioning and dunnage Unit container i..

Level C l"f Wrapping material Cushioning and dunnage Unit container Packing Level B Level C Marking for shipment

NOTES

CODE IDENT. NO.

11�47

APPROVED SOURCE(S) OF SUPPLY l

SPEC SUPPLIERS CODE !DENT FINAL

SUPPLIERS NAME AND ADDRESS

NUMBER PART NUMBER NO. PER H4-l APPROVAL DATE

232-11704-1

232-11704-4

232-11704-7

232-11704-11

232-11704-14

232-11704-17

232-11704-20

232-11704-25

232-11704-27 r----------"'----.- W"

232-11704-30

For detail component usage Assembly see

I l

I sheet 12

-30

-27

-25

-20

-17

-14

-11

-7

-4

-1

PART OR IDENTIFYING

REQD NUMBER

D1 4802 5060 ORIG. 3/71

per For continuation see sheet

Servo Assembly

Servo Assembly

Servo Assembly Engineering Model

Servo of

Assembly -------------.- ---- -- --i-·

Servo Assembly I

Servo Assembly Erigi neeri ng Model

Mockup, Servo ,l\ssemb l y

Servo Assembly Engineering Model

Servo Assembly DT&E Flight Unit

Servo Assembly

NOMENCLATURE OR

DESCRIPTION

PARTS LIST

Silt: CODE IDEN-;- NO.

81205

SCAL� I ..

Parts List

!IC>

IT9>

[D

[D [D

[D

[D

I 2 >

13 >

[D

MATERIAL AND SPECIFICATION

232-11704

D I SHl:::ET lO

IT:.>

[I>

NA

I l[I>

NA

NA

NA

[D

CL>

WT

!,ii

SOURCE OF SUPPLY

SPEC NUMBER

SUPPLIERS CAGE CODE

SUPPLIERS NAME AND ADDRESS

FINAL

PART NUMBER NO. PER H4-1 APPROVAL DATE

232-11704-34

232-11704-36

232-11704-38

232-11704-40

232-11704-42

232-11704-44

232-11704-46

-46 Servo Assembly [20> [4>

-44 Servo Assembly [18> [4>

-42 Servo Assembly [17> [4>

-40 Servo Assembly [16> [4>

-38 Servo Assembly [14> [4>

-36 Servo Assembly [13> [4>

-34 Servo Assembly [15.> [4>

QTY PART OR IDENTIFYING

NOMENCLATURE OR DESCRIPTION MATERIAL AND SPECIFICATION WT

REOD NUMBER

PARTS LIST

CAGE 81205 SIZEA DWG NO. 232-11704 SH 10.1 REVH

l

...I.

APPROVED SOURCE(S) OF SUPPLY I

SPEC SUPPLIERS

NUMBER PART NUMBER

232-11704-2 2117580-2-1

232-11704-3 2022 27 0-7-1

232-11704-5 2101796-2-2

232-11704-6 2022210-2-1

232-11704-8 2101796-1-1

232-11704-9 2022210-1-1

232-11704-10

232-11704-12 2101796-2-1

232-11704-13 2()22210-1-2

232-11704-15 21017%-2-1

232-11704-16 2022210-1-2

-16

-15

-13

-12

-10

-9

-8

-6

-5

-3

-2

REQD

PART OR IDENTIFYING

NUMBER

o - - I-, �

CODE IDENT FINAL

NO. PER H4-1

SUPPLIERS NAME AND ADDRESS

APPROVAL DATE

70210 AiResearch Mfo. Co. of r.al. Torrr1nce- r.a _ 9-9-83

70210 AiResearch Mfg. Co. of r.;i l . Tnrr.:inrP (';:i

70210 AiResearch Mfg. Co. of Cal. Torrance, Ca.

70210 A.i Research nfq. Co. of r;i l Trirr;:in;P r .:i A.iResearch Mfg. Co. of

70210 Cal. Torrance. Ca.

70210 AiResearch t1fg. Co. of Cal. Torrance. Ca.

70210 AiResearch Mfg. Co. of Cal. Torrance. Ca.

70210 A1Reaearch r•itg. Co. of Cal. Torrance, Ca.

70210 A lResearch rng. co. of Cal. Torrance, Ca.

7()210 A1Research rng. co. ot Cal. Torrance, Ca.

Actuator, [D Enoineerinq Model NA

Electronic Controller, [I) Enaineerino Model NA

Actuator, Mockup CD NA

Controller, Mockup [I) NA

Fixture, Test [D NA

Actuator, [D NA Engineering Model

Electronic Controller, I 2 > NA Engineering Model

Actuator, Electro-Mech- [D o=> anical, Linear ATU-88A

Controller [[) [D Actuator DCU-227A

Actuator, Electro-Mech- CD CL; anical, Linear A TU-88/ A

Controller, Actuator

IT> CL> DCU-227/A

NOMENCLATURE OR

DESCRIPTION

MATERIAL AND SPECIFICATION WT

PARTS LIST

SIZ!=: CODE IDENT NO.

81205 232-11704

SCALE I

F ISHEET \ )

iii

APPROVED SOURCE(S) OF SUPPLY I

SPEC

NUMBER

232-11704-18

232-11704-19

232-11704-21

232-11704-26

232-11704-28

232-11704-29

232-11704-31

232-11704-32

232-11704-33

232-11704-35

?32-11704-37

SUPPLIERS

PART NUMBER

2117580-1-1

2022210-6-1 20222Hl-3-l

2022210-4-1

2101796-2-3

2022210-5-1

2117986

2022914

2022210-8-1

-37

-35

-33

-32

-31

-29

-28

-26

-21

-19

-18

REQD

PART OR IDENTIFYING

NUMBER

CODE IDENT

SUPPLIERS NAME AND ADDRESS

NO. PER H4-l

7021() AiResearch Mfg. Co. of 1r;i1 TnrrPnrP f;i

70210 AiPesearch Mfq. Co. of r:al. TnrrPnfp ra.

70210 1\1r1esearch nrg. Lo, or Cal. Torrence, Ca.

AiResearch Mfg. Co. of 70210 Cal. Torrence, Ca.

70210 ACi�eseacch Mfg. ce. ofa . 1orren e� .a.

IAl Ke search Mfg. Co. of

70210 Cal. Torrence, Ca.

1-11Kesearcn rng. LO. OT

70210 Cal. Torrence, Ca.

KlKesearch nrg. Lo. or

70210 Cal. Torrence, Ca.

70210 AiResearch t1fg. Co. of Cal . Torrence. Ca.

Controller, Actuator

DCU-227/A

Actuator, Electro-Mech-anical, Linear ATU 88/A Actuator,Electro-Mechan-ical, Linear,Trainer Uni1 Controller, Actuator, Trainer Unit Actuator, Electro-Mech-ical, Linear ATU-38/A Controller, Actuator

DCU-227/A

Actuator, Electro-Mech-anical,Linear ATU-88/A Electronic control Jer Engineering Model Actuator, Electro-Mech-anical ,Linear ATU-88/A Actuator, Electro-Mech-anical ,Linear ATU-88/A Controller, Actuator

DCU-227/A

!_I_3,)

1 1s'\ -iJD

[I?_)

ITI>

IT[>

112:>

[D

[I>

FINAL

APPROVAL DATE

l 4 --,\ r- -, 14 ) I - _, r-lI>·

[D

II>

NA

G>

[I>

NOMENCLATURE OR

DESCRIPTION

MATERIAL AND SPECIFICATION WT

PARTS LIST

SIZE CODlc IDENT NO. 232-11704 A 81205

SCALE I F I SHEET 11.1

SOURCE OF SUPPLY

SPEC NUMBER SUPPLIERS CAGE CODE SUPPLIERS NAME AND ADDRESS

FINAL

PART NUMBER NO. PER H4-1 APPROVAL DATE

232-11704-39 2117580-3-1 70210 Ai Research Mfg. Co. of Cal. Torrance, Ca.

232-11704-41 2117580-4-1 70210 Ai Research Mfg. Co. of Cal. Torrance, Ca.

232-11704-43 202221 0-9-1 70210 Ai Research Mfg. Co. of Cal. Torrance, Ca.

232-11704-45 2022210-10-1 70210 Ai Research Mfg. Co. of Cal. Torrance, 9-9-83 Ca.

232-11704-47 2022210-10-2 70210 Honeywell of Cal. Torrance, Ca.

-47 Actuator, Electro-Mechanical, Linear [20> [4> ATU-88/A

-45 Actuator, Electro-Mechanical, Linear [18> [4>

ATU-88/A

-43 Actuator, Electro-Mechanical, Linear [17> [4> ATU-88/A

-41 Controller, Actuator DCU-227/A [16> [4>

-39 Controller, Actuator DCU-227/A [14> [4>

QTY PART OR IDENTIFYING NOMENCLATURE OR DESCRIPTION MATERIAL AND SPECIFICATION WT REQD NUMBER

PARTS LIST

CAGE 81205 SIZEA DWG NO. 232-11704 SH 11.2 REV H

_J w V, 2 I ·I

-17 -14 -11 -7 -4

-1

Assembly

.... =------�--u-=• •--•

-19

I -18

-17

-16

-15

-14

-13

-12

-9

-8

-6

-5

-3

-2

-11

-7

-4

-1

Part Number

Parts

SIZE CODE !DENT. NO.

A 81205

SCALE

1�.EY

Actuator

Electronic Controller

Servo Assembly D [D

Actuator, Engineerinq Model Electronic Controller Enqineerinq Model Servo Assembly NA D Engineering Model

/\ctuator, Mockup

Contro1 ler, Mockup

Actuator, Engrg. Mod.

Electronic Control-ler, Engrg. Mod.

Actuator DT&E Flt. Unit

Electronic Control-ler, DT&E Flt. Unit

Jl.ctua tor

Electronic Controller

Servo Assembly, NA fD Mockup

Servo Assembly NA (D Engrg. Model

Servo Assembly @=) D DT&E F1t. Unit

Servo � 15 ) Assembly __ __,, Description Wt. Note

List

232-11704

C I SHEET \� ....... -... �

c2 w f f-w

VI

:::i

_ ... "7'0... ...... -............. ..,_ .. --.c.-. '."=

2 i 2

I !

! I l I 1 1

I ! i

I i

I ---· - I

I

I

! i - I I I I

I

I i i

-37 Electronic Controller DT&E Flight Unit

-36 Servo Assembly DT&E Flight Unit

-35 Actuator

-18 Electronic Controller

-34 Servo Assembly --��- L,--,....... _____ ·---"---

-31 Actuator DT&E Flt. Unit

-30

-29

-28

-27

-26

-25 I !-----• • -•••L ••4-• - ----- .. ----------�--

-21

Servo Assembly DT&E Flt. Unit

Electronic Controller DT&E Flt. Unit Actuator DT&E Flt. Unit

Servo Assembly IDT&E Flt. Unit [Electronic Controller I Engineering Model ,servo Assembly Engineering Model -· ,Actuator DT&E Flt. Unit

Q)

Q) i�

DD

G)HI[:

I

NA (])

-l-- - I

I

-20 Servo Assembly [D CE>J - DT&E Flt. Unit

I ·----�-----------

! I 2 -16 Actuator l l Engineering Model

1 I -5 Electronic Contra ll er I DT&E Flt. Unit

I I

-36 -34 -30 ).-27 -25 -20 ' Part Number Description NOTE I Wt.

j I l

Assembly Parts List

SIZE CODE IDENT. NO.

A 81205 232-11704

SCALE REV E I SHE ET

l _ _J_

12 .1 -- - _.,._,,_., �-�--·----------.=-------···-�----�=---- D1 4316 2000 REV, 4/73 J \!",.,v�7

2 -47 Actuator [4> [20>

. -46 Servo Assembly [4> [20>

2 -45 Actuator [4> [18>

. -44 Servo Assembly [4> [18>

1 1 1 -2 Electronic Controller

2 -43 Actuator [4> [17>

. -42 Servo Assembly [4> [17>

1 -41 Electronic Controller

. -40 Servo Assembly [4> [16>

1 -39 Electronic Controller

2 2 -35 Actuator

. -38 Servo Assembly [4> [14>

-46 -44 -42 -40 -38 PART NUMBER DESCRIPTION WT. NOTE

ASSEMBLY PARTS LIST

CAGE 81205 SIZEA DWG NO. 232-11704 SH 12.2 REV H

z

UJ

I-z w

0...

c u..

w V'I

::J

1 SCOPE

l.� Scooe. The Servo Assembly applies torque to and positions the elevens to provide directJonal control and stability of i'light to the missile.

1.2 Classification. Not applicable.

SIZE CODE IDENT. NO.

A 81205 232-J.l'TOl-.

Cl1 4316 £000 REV, 4/73

J 13-0-47

2. APPLICABLE DOCUMENTS

2.1 Government documents. The following documents of the exact issue shown form a part of this specification to the extent specified herein.

In the event of conflict between the documents referenced herein and the contents of this specification, the contents of this specification shall be considered a superseding requirement.

SPECIFICATIONS:

Federal

L-P-3780 ( 1) 21 December 1973

QQ-P-416C (1)

21 September 1972

PPP-B-636H (1)

8 April 1977

PPP-F-320D (3)

17 October 1973

PPP-C-843D

11 July 1977

TT-E-527C

4 March 1969

Military

MIL-B-50878 (2)

31 August 1970

MIL-8-83050B

14 July 1969

MIL-C-8956 (1)

22 May 1972

MIL-C-38999F

Supp. 1 1 December 1975

MIL-C-45662A

9 February 1962

S12E

A

Plastic Sheet and Strip, Thin Gauge Polyo1efin

Plating� Cadmium (Electro Deposited)

Box, Fiberboard

Fiberboard, Corrugated and Solid Sheet Rock and Cut Shapes

Cushioning Material, Cellulosic

Enamel, Alkyd Lustreless

Bonding, Electrical and Lighting Protection for Aerospace Systems

Bolt, Self Retaining, Impedance Type

Military Specification Clamps, Loop, Tube Support

Connectors, El ectri cal , Circular Miniature, High Density, Quick Disconnect

Calibration System Requirements

CODE !DENT. NO.

81205 232-11704

L� -- - �---�·- -�,·--··· SCALE

Dl 4316 20cc ,'< EV, l!/73 u.

LU

2.1 Government documents (Continued)

SPECIFICATIONS

Military (Continued)

MIL-C-832868 (1)

18 June 1975

MIL-D-1000

1 March 1965

MIL-E-60510 (1)

5 July 1968

MIL-E-8189H

31 October 1975 Appendix A*

MIL-E-25366D

26 June 1974

MIL-F-7179E (1)

19 September 1974

MIL-F-14256D (1)

10 June 1975

MIL-H-46855A

2 May 1972

MIL-I-8500C (1)

3 May 1972

MIL-M-38510C

1 March 1976 Supp 1 7 June-1976

MIL-M-45202B

3 October 1968

Coatings, Urethane, Aliphatic Isocyanate, for Aerospace Application

Drawing, Engineering and Associated Test

Electrical-Electronics System Compatibility and Interference Contro1 Requirements for Aeronauti ca 1 Weapons Systems, Associated Subsystems and Aircraft

Electronic Equipment, Missiles, Boosters and Allied Vehicles, General Specifications for

Electrical and Electronic Equipment, Guided Missiles, Installation of General Specification for

Finishes and Coatings, General Specification for Protection of Aerospace Weapons, Structures and Parts

Type R or RMA Flux, Soldering, Liquid (Rosin Base)

Human Engineering Requirements for Military Systems, Equipment and Facilities

Interchangeability and Rep1aceability of Component Parts for Aircraft and Missiles

Microcircuits, General Specifications for

Magnesium Alloy, Anodic Treatment of

* Appendix A applicable for -l,-17,-34,-38,-40,-42, and -44 units only.

SIZE CODE !DENT. NO.

A 81205 232-11704

SCALE IREV F I SHEET l5

UJ

Vl

2.1 Government documents (Continued)

SPECIFICATIONS

Military (Continued)

MIL-N-25027D

24 July 1969

MIL-P-116G (1)

24 August 1977

MIL-P-23377C (2)

31 May 1974

MIL-P-26514E

10 May 1978

MIL-P-28809*

21 March 1975

MIL-P-55110B (2)* [- 19>

18 April 1969

MIL-P-55640A (2)*

4 April 1975

MIL-S-7742B (1)

Notice 2 15 March 1973

MIL-S-8879A (1)

Notice 2 15 March 1973

MIL-S-19500E (4)

Supp lG 2 February 1976

MIL-S-45743C*

15 January 1969

MIL-S-81733B (AS)

7 June 1976

MIL-T-83399

22 November 1974

MIL-W-5088F

30" June 1976

MS 9006C

20 June 1963

MS 21224B

15 April 1974

Nut, Self Locking

Preservation, Methods of

Primer Coating Epoxy Polymide, Chemical and Solvent Resistant Polyurethane Foam, Rigid or Flexible for Packaging Printed-Wiring Assemblies

Printed Wiring Boards

Printed Wiring Boards, Multilayer ( Plated-Through Hole) Screw Threads, Standard Optimum Series, General Specification for

Screw Threads, Controlled Radius Root with Increased Minor Diameter, General Specification for Semiconductor Devices, General Specification for

Soldering, Manual Type, High Reliability, Electrical Connections, for Missile System, Procedures for Sealing and Coating Compound, Corrosion Inhibitive Test for Removal of Flux Residues

Wiring, Aerospace Vehicle

Recesses-Cross, Low Torque Drive Dimensions and Gage Dimensions for Nut, Self-Locking, Castellated, Hexagonal, Counterbored

* Applicable for P/N 232-11704-l,-17,-34,-38,-40,-42, and -44 only.

SIZE CODE ID ENT. NO.

A 81205 232-11704

SCALE IREVG I SHEET 16

n, .4� IF. :;innn RFV. �;7-::,.

JI !':.O 47

z

2.1 Government documents (Continued)

SPECIFICATIONS

Military (Continued)

MS 21244A

7 December 1973

MS 33602

27 October 1967

MS 33750E

8 June 1971

MS 33787A

7 December 1973

STANDARDS

Federal

FED-STD-595A

2 January 1968 Change 4 1 August 1974

Military

MIL-STD-IOOA

1 October 1967

MIL-STD-129H

Notice 1 1 November 1978

MIL-STD-130D

5 March 1971 Change 3 1 August 1973

MIL-STD-1438

12 November 1969

MIL-STD-198C

10 December 1971 Change 12 7 July 1975

MIL-STD-794D

Change 4 8 August 1975 n1 .d.�1,=, -::ir.nr. i::lF="V .d./7-::a.

Nut, Castellated, Hexagonal, Counterbored

Bolt, Self-Retaining, Aircraft Reliability and Maintainability, Design and Usage Requirements for

Recess, Hi-Torque, Dimensions of Recess Gage and Driver for

Wrenchi:ng Element, External Spline Dimensions for

Col or

Engineering Drawing Practices

Marking for Shipment and Storage

Identification Marking U. S. Military Property

Specifications and Standards, Order of Precedence for Selection of

Capacitors, Selection and Use of

Parts and Equipment, Procedure for Packaging and Packing of, SIZE CODE IDENT. NO.

A 81205 232-11704

SCALE IREV D I SHEET

J1�•1'7

2.1 Government documents (Continued)

STANDARDS

Military (Continued)

MIL-STD-199B

4 June 1974 Change 3 28 June 1976

MIL-STD-275C

Notice 3 18 February 1976

MIL-STD-415D

1 October 1969 Change 1 8 October 1971

MIL-STD-454E

1 March 1976

MIL-STD-461A

1 August 1968 Notice 3 1 May 1970

MIL-STD-462

31 July 1967 Notice 2 1 May 1970

MIL-STD-483 (USAF)

31 December 1970 Change 1 1 June 1971

MIL-STD-490

30 October 1968 Notice 1 1 February 1969

MIL-STD-701K

26 May 1976

MIL-STD-704A

9 August 1960 Notice 3 11 April 1973

MIL-STD-7818

15 November 1967 Change 1 28 July 1969

I

01 4315 2000 REV. 4/73

Resistors, Selection and Use of

Printed Wiring for Electronic Equipment

Test Provisions for Electronics, systems, and Associated Equipment, Design Criteria for

Standard General Requirements for Electronic Equipment

Electromagnetic Interference Characteristics, Requirements for Equipment

Electromagnetic Interference Characteristics, Measurement of

Configuration Management Practices for Systems, Equipment, Munitions, and Computer Programs

Specification Practices

List of Standard Semiconductor Devices

Electric Power, Aircraft

Reliability Tests: Exponential Distribution

SIZE CODE ID ENT. NO.

A 81205 232-11704

SCALE IREV C I SHEET

_,-L.

---- �,m\

J!�47

2.1 Government documents (Continued)

STANDARDS

Military (Continued)

MIL-STD-810C

10 March 1975

MIL-STD-834C

1 March 1974 Change 1 10 December 1974

MIL-STD-889A

5 May 1972

MIL-STD-961

22 September 1975

MIL-STD-1472B

31 December 1974 Change 1 10 May 1976

MIL-STD-1495*

Notice 1 18 May 1976

MIL-STD-1515

2 October 1972 Notice 4 9 January 1976

MIL-STD-1568

18 November 1975

OTHER PUBLICATIONS

Manuals

AFSCM 81-1

18 October 1971

Regulations

AFR 73-1

30 Apri 1 1975

Environmental Test Methods for Aerospace and Ground Equipment

Packaging Data Forms, Instructions for Preparation and use of

Dissimilar Metals

Outline of Forms and Instructions for the Preparation of Specifications and Associated Documents

Human Engineering Design Criteria for Military Systems, Equipment and Facilities

Multilayer Printed Wiring Boards for Electronic Equipment

Fasteners Used in the Design and Construction of Aerospace Mechanical Systems

Materials and Process for Corrosion Prevention and Control in Aerospace Weapons System

Specification and Standards Manuals

Defense Standardization Program

*Applicable for P/N 232-11704-l,-17,-34,-38,-40,-42, and -44 only.

SIZE COOE IDENT. NO.

A 81205 232-11704

SCALE E F I SHEET 19

:wex...-

D 1 43 1 6 2000 REV. 4/ 7 3

J 13..(),47 o<

LU

UJ

V'l

2 .1 Government documents. (Continued)

OTHER PUBLICATIONS

Handbooks

AFSC DH 1-2

20 February 1974-

AFSC DH 1-3

Rev. 3 1 January 1972

MI L-HDBK-5

Vo 1. 1, Vo 1 . 2 1 September 1971 Change 4 29 August 1975

MI L-HDBK-17A

Pt. 1 January 1971 Notice 1 1 September 1973

MIL-HDBK-17

Pt. 2 14 August 1961

MIL-HDBK-23A

30 December 1968 Notice 3 19 June 1974

MIL-HDBK-217B

20 September 1974 Notice 1 7 September 1976

General Design Factors

Personnel Subsystems

Metallic Materials and Elements for Aerospace Vehicle Structures

Plastic for Aerospace Vehicles Part 1 Reinforced Plastics

Structural Sandwich Composites

Reliability Prediction of Electronic Equipment

...J z

LU

z

UJ

c u..

UJ

Vl

::J

2 .1

Government documents. (Continued)

OTHER PUBLICATIONS

Miscellaneous

ALCM Document 239B 1 April 1978

MIL-BUL-147

16 November 1973

SIZE

A

Parts Control Plan

Specifications and Standards of Non-Government Organizations Released for Flight Vehicle Construction

CODE IDENT. NO.

81205 z w

I-w

I I-w

V'1

2.2 Non-government documents. The following documents of the exact issue form a part of this specification to the extent specified herein. In the event of conflict between the documents referenced herein and the contents of this specification, the contents of this specification shall be considered a super seding requirement.

SPECIFICATIONS

The Boeing Company

0232-10337-1 (S) Rev. C

0232-10337-3* Rev. B

D232-10327-1 Rev. L

DESC Form 344 November 1973

STANDARDS

Not applicable

DRAWINGS

The Boeing Aerospace Company

232-11706 Rev. E

232-11707 Rev. F

232-11299** 14 April 1978 ADCN's 1, 2

OTHER PUBLICATIONS

Not applicable

Survivability/Vulnerability Specification for ALCM Procured Equipment (U)

ALCM Supplier Hardness Assurance Requirements

ALCM Part Selection List

Non-Standard Part Data Form

Actuator, Elevon Control, Outline Drawing

Controller, Elevon Actuator, Outline Drawing

Metal Core Printed Wiring Boards Multilayer (Plated-Through Hole)

**Applicable for P/N 232-11704-1,-17,-34,-38,-40,-42, and -44 only.

*Applicable for P/N 232-11704-1,-42 and -44 only.

01 "315 2000 REV. -1./73

ii"

LU

z w w V'>

::J

3 REQUIREMENTS

3.1 Item defin1tion. The Servo Assembly shall consist of two identical linear Actuators driven by a common electronic control unit. Each Actuator shall consist of an electric motor, reduction gearing, ball screw linear position transducer, and any other sensors required for functioning of the position servo. The electronic Controller shall consist of circuits to perform Actuator position signal summing, error signal amplification, servo loop compensation, power drive stages for the servo motors, current limiting, and bu.i'fer circuits to output position and motor current monitor signals.

The electronic Controller shall accept analog voltage inputs proportional to the eleven position command, 28 VDC power, and +15 VDC power. Cabling between the Actuators and Controller shall be a-part of each Actuator.

3.1.1

3.1.2

Functional interface diagram.

Interface definition.

Figure 1.

3.1.2.1 Physical interface. Each s�rvo Assembly shall comply with the interface requirements of 232-11707 (Controller) and 232-11706 (Actuator).

3.i.2.2

3.1.3

3.1.5

Electrical interface.

Ma.,j or components.

Item No.

Figure 2.

Item

Controller (1 each)

Actuator (2 each)

Government furnished property list. Not applicable, Government loaned property list. Not applicable.

3.2 Characteristics.

3.2.1 Performance. All 3.2.1 perf'ormance characteristics shall be met over the useful life of the Servo Assembly.

3.2.1.1 Angular displacement. The Actuator shall be capable of providing a true. angular displacement of the eleven of +14.0 degrees (eleven leading edge up; Actuator retracts) to -22 degrees, S:,e 3.2.1.8 for overtravel stop requirement within this envelope. The null of the elevon is zero degrees.

At null, the Actuator is perpendicular to the lever arm. See Figure 3.

SIZE CODE IDENT. NO.

I A 81205 232-11704 i..,,.,,.,_, IR_�� I SHE ETSCAL. E A. 22..

OJ 4310 2.000 REV, 4/7'.:: _J � S,..,.') .c 7

EI.EVON

POSITION

Ul r

COMMANDS

m rn f\)

(.n -I

;o

9 <

Ul I\)

I I m �

USE FOR DRAWINGS AND HAND PRiNTED lv\ATERIAL Ot�l Y - NO TYPEWRITTEN MATERIAL

28 voc POWER

EI.EVON,

'AC.WA'.l'OR CON'l'ROLLE:R ·•

.:_15 voc:'

• EtEVON ;coNTROL'

'iqvJ\TOR_

,-p�su11 ON I

:'.CO,MMJI.ND

\CCMWID; ' '

POSI'!'ION/ .. I

I ill

• ELEVON. ·

;coNr.L'ROL

II

I

'�CTUATOR;

FRICTION

COUPLING-

SfRING.

rrn -7 f--,ril- - � '. El.EVON l-4-- - - ,AERODYNAMIC 11W).

'.INERTIA

R

R

L--·_· ·-.:......:-�

EFERENCE VOLTAGE

MONITOR Sl'GNALS (POSITION AND MOTOR CURRENT) j

TEST SIGNALS (TO BE PROVIDED.BY SUPPLIER)

EFERENCE VOLTAGE

'1 RH� -7

r'4-- - � ; Ell."VO..'i r-- - - L �RODYNAMIC •. L9AD.�

L� ���A _J

-�OUPLING,'

SPRING

YHIC'l�ION

L--L--1------------------------r----------------------------'J�

J2

E LEVON

A ACTUATOR

H CONTROLLER A + REF VOLT

B

II 11

11 IIT

POT WIPER

SPARES N C -REF VOLT

I I s D I

E I

_, J3 I LJ LI

.::!: I "' Kw

I I - (L)A.CT CMD Ir I

� 54 B l z II ll(L)Ac.T RTN 11 C I

SPARES w

55 M 1P Pl

;:;:= N :3::

l(R)AC.T CMD w I a..

LJ � 52 D p 0 if) il(R ACT RTN E R z 53

L) 1P pi I I

>- T...J Li_ i(L) ELEV POS 55 F 11 il(R) ELEV POS -<l'.

G H } LEFf RHRACT ;; 59 w II ll(L) ACT C.UR

/4 � 50 p C, ii 1 1( R) ACT CUR a

7 R 5 ""I w

I .._:_ IQ Q I ) L£FT EXTEND .... z"' f:" a.. l I+ 1S VDC

_J t:::>z bO K <( II 11 - ,s voe J:

�j L a II II COMMON b2. M Jl } R.H, ACT T Vl SAME P..S J4 c., z C> ! l \3

-}SPARES a IZ O!

E TEST' ---6·-·

0 SPARES u..

F CO�NECTOR I

w

-SIGC:JRD V, I \ I ::J + A JS 5 -R FOSITION

>< 2 - L POSIT\OH

� Pi 7 R Ml"R CURRENl" Zr, C §8

I 1 10 l MTR CURRENT u> p D 8 R POT WlPER:z POT WIPER ::::, aJ 9 L --;N

CII::,._,, 4 R MTR YO LT I::! I- .3 1 1V\TR VOLT ►- L.

F\6URE 2 i ELECTRICAL l�\TERFACE

[:::> SHIELD TERM\ NAl"EO Silt: COD!:: ID!::NT NO.

c3Z-l l 704 A 81205 PERIP�ERALLY

SCALE REV C SHEET 24

z

<t:

w I-z -w I-c< a..

i'.:

c,:

w "' ::, � I _, , 3.2.1.1

Angular displacement (Continued)

The reference lever arm length is 3,00 inches, The extended and retracted lengths of the Actuator are shown in 232-11706.

Due to the reduction in effective lever a r m length at non-zero eleven positions Actuator force, displacement, and velocity are related to torque, angular position and angular velocity around the eleven a.xis as shown in Figure 3, SIZE CODE IDENT. NO.

A 81205 232-11704

L__ SCALE IREV I SHEET

i S"'

D1 4316 2000 RE\·, &/73

1,!"-£) .. 7 ex;

w I w 1-z ex;

z :r:

z

V, 0z u..

u.J

V, :J

:FWD

UPPER·

LIMIT.-

UP

:+l4°- '

-f3--

LOWER

LIMIT

0-22

G

G

TORQUE APPLIED TO ELEVON, IN-LBF

= ACI'OA'roR FORCE, LBF X 3.00 INCH AFM

VELOCITY OF EL.EVON, DEGREES/SEC

VELOCITY OF AC'IUATOR (IN/ SEC)

3.00 INCH ARM

X 57.3

POSITION OF_ Em/ON, DEGREES DISPIACEMENT OF ACTUATOR (Ill.GIES) .

;_:_; - - -- •• 3. 00 INCH ARM 1--- - - ---'

- -· ---- ------ -··· --- J

• X 57. 3 i

ATrACH 'ro STRU� u.'"'VER ARM = 3. 00 IN (REF)

,_ ELEVON

FIGURE 3 - COORDINATE CONVENTIONS AND DEFINITIONS

SIZ[; COD� IO[;NT NO.

A a1205

SCALE REV

232-11701+

SHEET '-.G.

....J w z w w c u..

w

V'I

3.2.l .2 Angular velocity versus torque. The energized Servo Assembly Actuator shall apply to or absorb torques from the elevons at values exceeding the limits shown in Figure 4.

3.2.1.2.1 Backdrive. The Servo Assembly, when energized, shall with-stand a steady torque from the elevon of +1500 in-lbf without being back driven more than 0.013 inches after application of load. (The nominal time duration is one second.)

3.2.1.2.2 Dynamic loading. The energized Servo Assembly shall withstand a sinusoidal loading described by the following equation:

Torque applied = ±6200e (.10�) CosWt, in-lbf w = 50 to 100 Hz

3.2. 1.3 Interface signal and power characteristics

3.2. l .3.1 Input command signal characteristics. The input command to the Servo Assembly will be a voltage which will represent an elevon deflection. The command signal shall have a voltage range of +7.00 volts to -11 .00 volts and a scale factor of 0.50 volts/degrees. For a zero command voltage, the elevon deflection will be zero degrees. The polarity of the command signal voltage is positive for positive elevon deflection.

Input command signals shall be accepted in the form of a differential input on two separate wires. The elevon zero degree position shall be referenced to the ±15 VDC supply return. The impedance of the Controller to the position input signal shall be 10 Kohm ±1 Kohm.

3.2.l .3.2 Position monitor signal characteristics. The Servo Assembly shall produce two DC analog elevon position signal voltages which will be monitored outside the Servo Assembly. The scaling of position monitor signal voltage to elevon position shall be 0.500 volts per degree. A positive output voltage shall correspond to a positive elevon deflection.

The position monitor signal voltage accuracy shall be within ±2% of value or ±9 mv, whichever is greatest. The position monitor signal voltages shall be referenced to the ±15 volt supply return and shall be O ± 100 millivolts with the Elevon at its null position (0 degree).

The Servo Assembly output shall be capable of driving a load of 5 Kohms or greater.

A short in the external circuit connected to the Servo Assembly or a malfunction in the position monitor circuit in the Servo Assembly shall not affect the performance of the Servo Assembly.

SIZE CODE ID ENT NO.

A 81205

D1 .4316 2000 REV. 4/"/3

z0

. C<:

a w � z

Q.

a a

-1100 -1000' -500'·

+150, +100

+50 .-

�50:

UNACCEPI'ABLE

,-100°/SEC ;_.,

- -960 :rn-tBF;

• -···- ····- - - - • __ .I

'.-100:

+500, z - . .,,_ <( , -200 :

z

1 sre] Ci w V, COID)ITIONS:

A. BASED ON FORCE IN MOUNTING BOLTS

B. SPEED IS CONST.A.lrr

C. + SPEED: ELEVON LEADING EWE RISES;

ArnJATOR REI'RACTS

D. + HINGE MOMENT: AEROMOMENT MOVES

FREE EI.EVON NOSE DO'l'iN

+loo0/SEC ..

+960 IN-LBF

·+1000· i_:i-l�Q_Q�

FIGURE 4, - TORQ� - SPEED CAPABILITY.

SIZ� CODE IDl=NT NO.

A a1205

SCALE REV C

232-ll704

SHEET � 8

z w � z w � i:'.:

ac:

w

V)

3.2.1.3.2. 1 Electrical/mechanical offset. Applicable for the -1, -17, -34, -38,-40,-42, and -44 Serv,o Assy .. only.· The Servo Assembly controller (-2 and -18) circuitry shall provide for a + 4.000 + .050 volt electrical offset of the actuator position feedback potentiometer signal at actuator mechanical null (0 degree). A short or open-circuit of this signal shall result in a position monitor signal greater than plus or minus 3.5 volts (for generating a 11 NO G0 11 in the FCSE).

3.2.1.3.3 Motor current monitor signal characteristics.

a. Two DC analog signal voltages shall be produced by the Servo Assembly, which are proportional to the two averaged motor currents. The signal voltages shall be referenced to the +15 voe common. The signals will be monitored outside the Servo Assembly.

b. The output voltage shall be scaled to 0.2 v/ampere of motor current.

A positive current is one which drives the elevon in a positive direction. The current monitor signal voltage accuracy shall be within +3% of value, or +100 mv, whichever is greatest. After nuclear radiation, the current monitor signal voltage accuracy shall be within �3.3% of value, or �200 mv, whichever is greatest.

c. The Servo Assembly output shall be capable of driving a load of 5 Kohms or greater.

d. A short in the external circuit connected to the Servo Assembly or a malfunction in the current…