Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
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TOP SECRET G 

-

Bl F-008- __ 0_19_8_4_2-_R_l_-_so 

lLO CUTTER SEALER AND ~1EClJA.i'Y ISMS 

"fhe PPS/DP F.AC contains four CT'S cat:Kup cut tcr, tvro 

tunnel seal and record traps ('fSlffs) t an<l two splicer meclJ,anlsms (splice tcrs), 

·rhcsc are all lng-- lm<dc:d 

Pe Part 3, 

-act.1i:1te<l flevJ ccs in the termJnation and 

12), 

11. 1 l:'unct ion 

Ctrttc:r/seaJcrs 1 an<l 2 a.re mounted on the capsE1 l c co·1tcrs of SRV 

rcsn,,,,1civc1y. V.'hen 

seal the ca:pstElc against 

cut any film not TolJcd Jnto t.he SRV, 

externu l envi ronmcnt~ 

3 and 4 and nso;cmbllns arc monn11ad in the 9 and S 

1'SRT cncJosurcs. The cut sealers act as Im-path 1 and pressure seals 

after t11e sn1:a1·atian of SRV 1, and a::> rodui:idtmt \.:Utters to C/S 1. '1110ir 10-

cutlun the tunn0l scp;u·w.tlon points ensures that lm trapped 

the tunnel will not scmHcction oF Che ejcctahlc utlaptc-r The 

TSl<Ts 1 cutter I ers with the h 

tween TSRT cnclost1rcs and 

seals for 

of any fi Jm trapped by the 9 TSRT 

shield J s mounted aft of the 

flln1 tu SRV 2. 

'fhe art ha c11tter {ABlJC) i::; a 

s 

and hold any film left beal so st:rvo as light 

lrn paths. 'l'o ensur0 that the free end 

not enter the fi. J m tu SRV 2, a 

;)4. 5 bulkhead between the 1'Sl\T and tfu:: 

r the 

moved. t-1ounted in the film s;1pply enclosure,. it ucts as a redundant cut tw r 

to C/S 2. 'fhe 9 5 rnechrinisms ore located in the fj lm s11pply 

3.11-1 

T~T t: 

Hardle 111n BYE.MAN 

Cortn,l Syst:rm Ori y 

Approved for Release: 2017/02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

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for Release: 2017102/14 C05097360 
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Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
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Approved for Release: 2017 /02/14 C05097360 
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Bl 

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Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017/02/14 C05097360 

~ET G 

Bl F-008- l\'-C-Vl9842~Hl-81) 

11,2.4 C<J t tcc/.~c,ulcr (fpcrat ion 

'fhi.~ ro11owing dJscussion refeYs tu P;i;ucc 

U]1on command, tl1c <lirnple motors in the la ng moc1tani~n1 arc actuated, 

The.' lov;er ls then released 

and the tors Jon sprint;s pul 1 thf' door free, The door is forced sl1ut tlte 

springs und the fj lrn ;;t.ran<l(;;) severed tlte knift: blade. Under norrnal 

loads the door 

lat,;.::hcs, which st1pp 

he :shut by thi:..1 ye:;:1dual force of the springs. 'l'wo 

a positive locking fo1·ce, are incJ udeJ to guard aga1 nst 

the effect of shoc:k loads or uthcr abnormal f"o1·ces. 

details of 1 mc,drnnism arc lllustrati:d in 3. 11-6 

through 3,11-fl. Ench splicer mcnsurcs upproxi111otely 5 x 7.S x 10 inclies 1 

and weighs aho11t 10 pounds. Po1• puxposcs 

been broken tlown into four suliusscrnblics: the i1yr0tcch:11c d:1 1c motors and 

i:hc sht1ttle assemhly, the platen assembly, the electricu1 

ronnet:tors nnd i:rs t ru1nent tt t ion. 

11. 3. 1 Dimple ?cJoLors und r: Linkage 

·rhe drive lrn"'agc,; illustrated in ,'i. ll-8, consists of tlte encoder 

sho ft,, the llrive shoft, and the cra11k bars pantograph arms. 

'l'he encoder shaft is 1: l to th1..•. drive The r1Jmentation encoder is mounted nt one end or the while at tlte opposite entl 

the 1;1tch l nnd lotch p.covide ho force octLiation control for 

::;plicor. ihe latch is relca"'d firing rcdcmclartt <liinple moto1·st el 

3.11-UI 

~G 

Approved for Release: 2017/02/14 C05097360 

Hal'\dlc 111;1 BYEMAN 

Ccrtr-:d Sys.tc.M 01'\l'f 

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Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017/02/14 C05097360 

T.C,P [ EC!a'T 

Bl F~OOS- h'·-C-019842-Rl 80 

which is capob of pr'ov ing :suffici0nt r th"' tasl'. Senarate f1ri.ng pulse:-; arc provided to each on twisted, shie1d0d wires from th0 

initiator 0lectronlcs unit. 

'l'0r:-; ion spr1ngs rnuunt0d on the dr1vc pruv1d0 energy for the ~+pl ici:ng 

oyicrntion. The drivlng force ls trnnsmittod to the encoder shaft throu~~h the 

rn2ting genrs, and to thv puntograrrh 1ink11gc two crank bnrs, one at ~;ach 0n<l 

or the ~+hrtft. U:s;: of the puntogr?ph ilTfl"l design tu the s11uttle Piotlon cn,:.ur0s thnt the shuttJe D~'scrnbly wi1J pres:.; squDrcly 0n tlte sμliclng 

plnt011, 

JJ,3.2 Shuttle Assemh1y 

The ly is a mctaJ stru(.·turt~ supporting l1tc upper b 

. c:tntionary b~udc on the lower str·11L',turr to sever the f't hn str'1nd fust artcr 

the pressur0 pad hus formed t1tc sp1i:.::e, At each end or th0 shuttle stru('-

ture 'rs A :-;otscrek' G.thich activntes n gato r0l0aS£' lever ofter the spl1c0/ct1t 

h2s bt~0n nccompl 1 sh0,1. 

ll,3.3 Platen i\ssorib1y 

'111e platen us~-;0rrtbJy is :.::0111poscd of the plat<~n hous " fi1rn guide rol lcrs, 

nnd gn. tc st ructur0. 'fhc pl 8 ten ass01nb 1 y holds the f 11 m 1 0Ad0r from SPV 2 

and provides u surfn:.::c upon i-vhich the shuttle asscmb 

and 1 ond0 r; ir tape. Thi~ plat0n hous 

ri 1rn .. gu1de ro1 ler;, and the gate structure. A speci.al ins0t on the h011s 

forms & pad against which a serrated vdge on th(..' c cl a.:mps tltc leader 

pos~ti.vn stop the 1eadf'r strand fro1c be 

pulled out of the splicer inadvertently {sco Figuro 3.11-9). FoJJr HStDblc 

l'e P 5ECRET -,.,£.... 

Approved for Release: 2017/02/14 C05097360 

!iatidle -Jia BYEMAN 

G:;mtrol Sy"-te111 Only 

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Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
• ~ epproved f~elease: 2017/02/14 C0509~0 T aJlo"SE CR ET 

IMP Des 

5517 l 2 2 s lH to Ifv1P SS ' monitors 

to the redundant pyre rn 

5538 C11t 3 1 Similar to IJ\.4P 5536 

5539 /Seal 3 ? Similor to IMP 5536, rnonl tors 

to redundant pyro in cut 

Cut/Sen i 4 1 lar bl IMP 5536 

eDl 4 2 Similar to IMP 55 ' monitors 

to the redtindant py1'o in c11t t 

5540 TSRT 5 l Similar to TMP 5536 

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~ 

5541 TSRT 5 2 5 to !MP 5 n1oni tors 

N ' to the in TSRT 

~ 

5542 TSRT 5 l Simll11r to TMP 55'.}6 

5511 :1 TSlff 9 2 Si111i lar to IMP 36, monitors 

to th(' 11yro in TSRT 

5530 Aft Bac,k1rp ter Simi lnr to TMP 553(> 

5531 1\ft 80 Cutter -' Siml lar to Ifl-1P ,!)536, monitors 

to the nt pyro l rt 

5534 5 Spl t Similo.r to IMP 

5535 5 i 2 Sln1ilar to T?,f P mon:! tors 

to the ant pyro in tho 

5532 9 ice/Cut 1 Similar to 11'1P 5536 

tlitr1d!e via BY EM AN 

Control Systrrn Only 

Approved for Release: 2017/02/14 C05097360 

81 • F-008- W-C-015842-Rl-80 • • 

Pov.rer 

fi pulse output +5 vdc 

::;ealer 2 

+5 vdc 

e fi pu 1 se output +S vdc 

sealer 3 

+S vdc 

the pulse 011t put +5 vdc 

sealer 4 

+S vdc 

the pulse 01Jtput +5 vdc 

5 

+S vdc 

f pt.tlse +S 

9 

+S vdc 

tl1e firing pulse output +5 vdc 

aft cutter 

,5 vdc 

the fl lse output +5 vdc 

5 sp11cer ism 

+5 vdc 
I-' 

I 

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Approved for Release: 2017 /02/14 C05097360 

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Bl 

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Approved for Release: 2017/02/14 C05~ 

.;:.tilf""!!' C R ET ...::.__ 

Jj.£' .• 3 Cut nnd Seal 2 Conuuand 

cirr A:\lD SEAL 2 {P02S77' P01577, P0'.}S77, fl-1P00062) 

Function: Actuates - cuttt'r/sealcr 2 

aft bBckt111 cutter 

3,ll-26 

~G 

Approved for Release: 2017/02/14 C05097360 

Bl F-008-

Kanrlle via BYEMAN 

Control System Only 

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Approved for Release: 2017/02/14 C05097360 

~RET Bl F-ooa-W-C:.1119842-Rl-80 

12~ 0 TEl1}11NATION AND RBCOVLRY 

The recovery of rilm is accomp1lsheJ hy ejection, deorhit, and 0val of 

the two satellite reentry vehicles {SRV1 

supported by the Jual recovery module (DRM) 

Prior to cction, the SRV's are 

portion of the PPS/DP EAC i.;hich 

contains fhe auxiliary cqt1ipment (filni tt1nnels, 1 s, etc.) for 

on-orbit operation a11d on conunan<l. 

Subsequent to on, the SRV is an independent system which m11st t 

satis dcorbit and atmospheric and must expedite rccovt..1ry 

catch or ~·atcr rctricv;ol), Each SRV pro·vidcs for monitoring transmission 

pertinent <loorbit/recovery events through two 

(Rf) beacons . 

12 .1 

le cons s SRV 1, 

ependcnt radio 

ectable adapter (EA), and 

the fixed adapter (FA), wJth SRV 2 moumtod within the FA. DRJl-1 also contains a11xi liary equipment for f i Im trans and SRV e j cct iont incl ud 1 ng; 

fllm tunnels~ the c1Jtter/seD1vr end TSRT mechanism, the blast shield and 

blast shield valve, pin-pullers and ection asoo,:iate<l teeconnection cabl 3 .12-1 il l11stratos internal configuration 

of the module. For a more 

Part 3, Section 1. 

1ed discussion of the components, refer to 

12.2 

Prior to execution of the M\i/TRANSFER/SEPARl\TE command seq11encc (12.3.1,3) ~ 

the SRV rema s sivc except for film takc-11ps, internal heaters, and 

3.12-1 

~.Tc 

Approved for Release: 2017/02/14 C05097360 

Handle via BYEMAN 

Ct.titre! Syil•~rr Or:l; 
Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
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fl 

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Approved for Release: 2017 /02/14 C05097360 
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T~T 81 F-oos-W-C-019842-Rl-80 

The co11tro! signal is removed from '1'/lJ 1 hy execution of the ROLL-lN TERt.1INA'IT'. (RIT) command. 

l 2. 3, 1 . 2 ClJ'f/SEAL 1 Conunnn<l. CUT /SEAL l conunand, no.rma l er 

the 9 RTT and 5 RIT conur,ands, activates the c11tter/sealer on SRV 1 (C/S 1), 

cuttcr/scalors in the 9 arid 5 'l'SR'f enclosures (C/S 3 arid C/S 4) 

and the TSRT mechanism::; (l'SR'i 9 arid "fSR1' 5) . :seal the SRV 

recovery and seal the film tunnels against light, and dcbri s from the 

SRV l retro-rocket, t'\dditior1ally, the cuttor/::;calcrs will cut any 1111 riot 

ro11ed onto tl1e T/lJ s' tho TSRT mechanisn1::; will c. and hold any 

lm left in the lm ti1nnel between the 1'SRT' s a11d sp1 icers to ens11re that 

it cannot jeo1>ardize tho second half of the mission. 

12,3.l,3 EPSM l ON Comrna11d, 'fhc SRV 1 reco"VcTy battery heaters (EPSM l) arc 

normal Jy commo.Jtded OK four revol11tio11s (three revolutions mini.mun:) JJTior to 

SRV cctio11 to establish the proper operating ten1peraturc for battery actvoltage level wd not be reached within the required time for SRV 

subsvstcm opcrat ior1. 

12,3.1.4 .A,R!11/TR/\NSFER/SEP!\RATE (ATS) Commands.* On the revoJ11tion, 

the PSV positions the SRV i11 the proper recovery attit11de (reference Section 12.2) 

and the SRV ectcd e.'(ecution of the ATS corrtr.1and sequence: 

1) ARM 'lhe .A,fl.}·1 command activates the recovery battorie::;, 

t110 SRV programmers and event beacons 

starts tho r0covery hack-up timer. 

TRAKSFER 1.8 seconds** prior to sepa ~ the 'l'R.i\NSfER 

s on 

**Actuo.l value::; are 

command activates the SRV thermal batteries and infli;::ht disconnect l • l\ lar:yar<l pulls 

the loose If.D cable clear , simultaneously 

rel cu::; tho blast shield valve. Separation of 

IFD breaks an electrical ground through the connector. enablin.g tltc SRV dual ejection 

sequence, see Section 12.10: Command Sununo.ry 

hy GE RESG. 

::l.12-10 

TOP 5 i!E!REr G 

--- -

He,.,::lle v1 e BY EM AN 

Co1tru1 $y$t<:m Grly 

Approved for Release: 2017/02/14 C05097360 

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~RET c 

12.3.2.2 SRV 2 ection~ SRV 2 J s sealed upon execution of the ctrr/SLAL 2 

• 

commRnd,. ac vating ler mechanJsm mounted on the SRV (C/S 2) 

along with tlte backup cuttcx·. Norn1ally,. CUT/SEAL 2 wlll not be c.ommand- • 

e<l u11ti1 all 

SRV 2 ejection 

eovery bat 

rema:ining fi ln1 (both 9 an<l has been ro11eU Jnto SRV 2, 

11ow$ swne procetl1Jre as des er lbetl SkV 1. The reheaters (LPS1'1 2) are turner! on a s11rfici ent tirae prior to 

sena·rai:ion to ilize the battery temperatures,. and the normal AA'-1/'fRANSPER/ 

SEPARATE command exe F igute 3. 12-4 an<l 'fables 3, 12- 1.<i and 

3. 12-lB si.1mmo.rize th.e ection :in<l recovery sequence for each SR\r, 

3.12-12 

TOP SECRET G 

Approved for Release: 2017/02/14 C05097360 

f{D.ndle v«;i BYEMAN 

V:mtrol Sy~t"rr Only 

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Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017/02/14 C05097360 

;,)'; t] !'c1 r\za1 

;}j f,'GMN'Cl 

EMAN 

?\((\;;,,J,:od \fV 

:wys,;,1 ni> 

H~((f !"'"'''"''") ;f 

HF 2\\ ;(('••('\\') 

""• A Approved for Release: 

ko\ r:r <o:Xet 

f' "" 

3. J 

"fl' 

(i\1 

;.;>Ht r.o:f) 

A 

2017/02/14 C05097360 

Bl 

f'.r1·y1;1". /,•corn·0:1. 

"' 'hru1l vd\\' t1rn tC l'•J7t ,'O'H 

ii""' ·,"''\¢' 

f\Jtn•\"O 

of Events 

\} 

1h0(\1' d\\1tW 

(·L·$$0?'1: f.>Y1'4;b)·, 

·t;r·•.tr:i.•r:. 

~ti' 3'\'""" f\0}1' 

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d}«P ,, (Uik 

!:~:~::~::. init11tted 

'/\Cf J'H: •JJ 

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Approved for Release: 2017 /02/14 C05097360 

Bl 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

1 

+ 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
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Approved for Release: 2017/02/1~ ~0-509.L: 

T~ECRET 

81 F-008-. W-C_:Ol98.42-Rl-80 

ing the spin :rate so thJ.t the aerodynnmic encountered 

cart rcori ent tl1e vcl1i c1 c att 1 tude. l1av1 ng coinp 1 eted 'its 1 the thrust 

cone (TIC) port1on of the SRV is then ejected and the :recovery programmer 

assumes control. 

Upor1 reenter1 the Ea rtl1 ts atJnosphert::. t11e cle attains a nose- attitude, wit!: the heat shield protect tl1e recoverable capsule. As the deceleration force increases,, the G ·1:.:.:hes close, lbitlng the ba\.:kup 

sequence. When the force ses, the G swit rcopf:n and the mary 

timers of tlte recovery progrannner are enabled • 

. !\pproxin\ately 26 seconds after 

the aft end of the reentry 

programmer ;;tarts~ the therma] cover on 

cle is ejected, deploying drogue parac}rute. 

and the fo:rf'hody is :released. nm 1 n e ls t1ten depl a 

condition, dere2fed, and the su1c descends on a f1Jl1y· hlossome-d parachute 

ur1til cau;:ht hy tl1e recovery aircraft. 

Ir1 event that tl1e G switches do not inhibit the recovery p:rogramrr~er bao:.:kup seqtuer1cc; t'he backup scrrucr1cc \4i 11 

the RV 2068 seconds after ARM. 

e device$ rcleas g the thrust cone 

ckup sequence wi 11 fire 

the pyrotechnic devices 

2808 »<"cortds after ARM. 

scpcrati11g t}ltc' thurma1 cover fro1n the 

Ni th parachute deplm1ncrtt taking p1 ace prior to or during 

the h1 gh atmospt1eric heati and capsule will be dcst.rc•yr>d 

by ae:rodynan1ic heat • 

Should tl1e s111e land jn water (;;ieria1 recovery unsuccf':ssful) J is weighted 

to float nose: down. 'fhe recovery beacons 11 continue to transm1t until the 

batteries are Tf tlu: st1le has not been retrieved within 40 hours 

(no111inal time)~ a d:issolvnble plug in the ;1ose will allow flooding and ;;inkto prevent unauthorized recovery of the film . 

:S.12-21 

Approved for Release: 2017/02/14 C05097360 

fLi~dl.:; V•B BYEMAN 

Contrvl Sy~ti;m Ord r 
Approved for Release: 2017 /02/14 C05097360 

RET _ 

1 

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R 

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~er~roved for !!.ase: 2017/02/14 C050973@Ji • 

ESM 

Hand! & vi a Ctlrrsulc 

COntrol Syatem Onty 

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RET 

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T 

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RET 

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61 F-OOS- -"-'"-".0.:1 '::J s~_l-_a_o. 

TJTLE 

5109 f'BM* for TEU 

51 mu (' 

5117 CllM 

A* i t 

***Most Signifj cant Bit 

***Ar1

1\11 t-o side A input c 

the , mori or 

the of commantls the satellite 

control sect Four :relays a resistance 

network form a converter who!'!e 

( Jiscrctc rang 

0.2.S volt to 4.75 volts in 0.3-volt incrL'mcnts: 

Bit 1 ( 

2 

Bit 3 

Bit 4 

in t!1c ILU 

)** -

- )*** -

-

TRANSFER 2A**** 

ARM 2A 

TH.Ai'ISFDR IA 

ARM 

0

-a A A 

"Approved for Release: 2017/02/14 C05097360 • 

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+15 

+S vJc 

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for Release: 2017102/14 C05097360 
~ECRET 

IMP 

556'1 

55()5 

5508 

• '" 

~ 5509 

N 

' "' a 

Approved for Release: 2017/02/14 C05097360 

G 

TAELE 3,12-~ (CONT'D) 

'd) divider circuit outtrnv out 4.0 volts 

aratPd). Th.;; 

resulting in a bi 

SRV 1, ion -Y 

SRV l, ration +Z J 

SRV 1, Sep a rat ion +Z 2 

"011 = Not Hl!J ::: 

Simi I ar to Il'<iP S564, 

is ti:::ed by the DTU, 

sign::l: 

is mounted 

00 the forw:1rd EA ring near -L 

Simi lnr to IMP 5500, monitors 

pt11 se output to i1yro l +Z llor. 

Similar to !MP 5500, monitors the og 

se output to pyro 2 the +Z ller. 

+5 

+S 

t5 vdc 

5510 SltV 1, ion z 1 Sirnilar to lMP 5500, mDnltor~ +5 

se output to pyro 1 for the -Z pin-11ul 

l SRV I, -Z 2 lar to IMP 5500$ +S vtlc 

pulse to pyro 1 er. 

5566 2 iori +Y Similar to !MP 5564, the !' l is attached +15 v<lc 

to 2 n1ount 1n RA nenr +Y, 

5567 SRV 2 1on -Y s IMP ,. J t110 plunger is attached, +5 vdc ' 2 movntJ11g ln the FA near -Y, 

5512 SRV 2, +Z 1 Similar to !MP 5500, monitors the +5 vdc 

pulse t to pyro l +Z Jer, 

HMd!e "ia BYEMAH Co. s,,,.,. ""'• - - ~pproved for Release: 2017/02/14 C05097360 • 
___________________________ _ 

Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

B 

1 

Approved for Release: 2017 /02/14 C05097360 
• • • • ~ .pproved f~elease: 2017/02/14 C0509~0 T~CRET __:._ Bl F-008- 9842-Rl-80 

5518 

5519 

5520 

5521 

5522 

5523 

5003 

Hilrldle 11i<1 BYEMAN 

Control S~sfmi Orll y 

l'.A Separation 156 degrees, 

l 15 vdc 

EA Separation 36 degrees 1 

EA Separation 156 degTces 2 

EA Separation 276 degrees l 

EA Separation 276 degrees 2 

Envir0::im:n1t11l Br:.inch 1,2,4, 

lng Brake On/t)ff 

TAllLI' 3.12-3 'D) 

milar to tMP 556'1. The plunger 

attached to the forward edge of 

approximately 156 degrees, and 

.;'{side of the pin-p1111er. 

is 

FA at 

on the 

Slmilar to IMP 5500, monitors the firing 

pulse outp11t to py1·0 l ror the FA pinpullcr lot.:atod at 36 degrees. 

Similor to fMP 5500~ monitors the firing 

pulse output to pyro 2 for the D1\ pin1Ju1 ler locutod at 36 degrees. 

Slmi lar to li'lP 5500, 1no11i tors 

puls0 output to pyro 1 for the 

puller located at 156 degrees. 

firing 

EA pin.-

Simi 1;:1r to IMP 5500, nroni tors the 

se output to pyro 2 for the EA 

puller located at 156 degrees. 

ring 

pinSimilar to IMP 5500, n:onito-rs the fi 

pn1se outpnt to pyre 1 for EA p 

puller lot.:atcd at 276 dt..•grees. 

lar to IJ't1P 5500, n1onitors the firing 

puls~ o-t1tput to PY"O 2 fol' EA pinpulleT· located at 276 

Latching T'clays tT1tcking the corrunand ir1put 

Ye1 of corrunand pr•OC\\SS:or monitor the 

receipt of commands from th0' sate11 co11-

trol section and feed either 0.0 volt or. 

s.o volt$ tu an int0grated circ11it D/A 

Approved for Release: 2017/02/14 C05097360 

P.QWER 

+ 15 vdc 

tS vdc 

+S vrlc 

+5 vdc 

+5 vdc 

+5 vdc 

+S vdc 

+5/±15 vdc 

G 
T~ET Approved for Release: 2017/02/14 C05097360 

_'2.- SI f-008- W-C-019842-Rl-80 

(Cont 1 d) 

EPSI>t 1, 

SS77 Environmental Branch 1 

Monlto:r 

5582 

3 

Hand!e via BYE.MAH 

Rnvi :ronmental Branch (1 Vol 

Monltor 

EPSfl-1 1 \to l Monitor 

TABLE 3.12-3 

converteT,, relays and one !f-bit Ll/A 

convcrtot 11'1P. Outpv t occ,urs 

s ccn(16) dJscrete ranging from 0.25 

volt to "1.75 vo in 0,3-volt incrcmi.:nts: 

B'it 1 (LSB) -Fnv. l 

Bit 2 " Er1v. Brancl1 2 On/Off 

t 3 " 5 ng On/Off 

Bit 4 (MSB) Env. Branch 4 On/Off 

Simi to TMP 5003: 

Rit 1 (LSB) - Env. Branch 5 On/Off 

Bit 2 Env. Branch 6 On/Off 

Bit 3 = EPS7'1 1 On/Off 

Bit 4 (MSB) = EPSM 2 On/Off 

A two- to:r vol t circuit connvctcd across branc11 1 l in 

the F~i and C monitors voltage level, 

bl 

is 

sl l 

11Q1t "' 

ir1•r "' On 

ti zed in the DTll to 

(On/Off). 

SJmllar to IMP 5577, monitor:> the 

in the P21 anti C. 

t:ld 

SJrn:llar to 

pOWt;r feed 

tMV 55 77, 111011 i tor~ t11c EFSM l 

tl:t: PJ\1 a C. 

a 

6 

11 s,,,~,,. • • 

Approved for Release: 2017/02/14 C05097360 • 

+5/:tlS vdc 

Self 

f 

Self 

G 

-. 
Approved for Release: 2017 /02/14 C05097360 

T 
Approved for Release: 2017/02/~4~~5/ 

,,,.ECRET ...JL 

Bl f-008- W-C-019842-Rl-80 

12. JO 

12.10.1 Splice and Cut Corrunand;,; 

9 SPL ANO 001766. P03766) 

5 SPLICE kND CUT (P025 POl 

Function: 

Interlocks: 

Comments: 

(al Act11vtes the mechani !'im OT 

(b) Connects t11e 9 5 control 

si ~ to -'-

9 SPLICLl AND CUT enables 9 ROLL-lN 

5 ANO CUT eJ'; 5 ROLL- TN TERMTNA1'E 

Fi Im lTillS t be stationary ex e comM 

Cb) on sl1ou1d 

after 

(c) After execution of 

tall of the lm must 

ln; is 1novc<l in 

thP 1 ce ::; n01cuv 

thln 10 minute 

f1 rs t 1 i cut, the loose 

be rolled into SW 1 before 

12.10.2 Roll-In Tc:rn1inatc Con1.mnnds 

9 ROLL- IN T~i~~:;~~;~~ (1102652, 5 RDLL-1?\ T (N02752, 

NO 

N01 

2, N03652) 

NO:l7S2) ' 

the 

1. 

cont ro ! from 

Interlocks: 

Com1Hents: 

9 ROLL-TN TL!lMINATE 

5 ROLL- IN 'Jl'.Rf.fINA'l'E 

oaublcd 

f'nttbled 

by 9 kND CUT 

S SPLICE AND CUT 

com:man<ls should no l be 

11n has been :i:olletl into SRV 1 

AND CU1'~ or S SPL i\ND ClJT. 

to ro! l eJ in are imatcly 

9 subsyston1 11 feet Lhe 5 

3,12-46 

~ET G 

until the 

nf1:cr 9 

lengths 

8,5 feet 

SUlbS)•Stem, 

cut 

tiar;a!<: ,,,n BYE.MAN 

C?ntn;rl Sjstc:n 6n1 y 

Approved for Release: 2017/02/14 C05097360 

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I I 

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l 

l 

l 

l 

l 

l 

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B 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017/02/14 C05097360 

G 

Bl 1-008- W-C-019842 Rl-80 

12.10,11 SRV 2 Trans 

12.10.13 

SR\1 2 TR.l\.i\SFF.R 

F11nction: 

Comments: 

(N02757, N01757, N037S7 > ~lNU0114) 

(a] Fires the 

batreries in SUV 2. 

(h) 

(a) 

type nvro;;1 

SRV 2 TRANSPER is enabled SRV 2 

thermel 

(h) SRV 2 eni;bles SRV 2 SEPAH1\TF.. 

Command fo1 low~ SRV 1 /\R\1 by 120 to 1992 

Se0o;rotion of IPD es the t'.h1a1 ect ion 

in 2. 

So;;e1:·oto Commar1d 

SRV 2 SEP.A.RATE 

function· 

Conunents: 

(N12000 .. Nl l 000, Nl 3000, M.c\001 l 7] 

1\ctustes pin-pullers releo:su:g SRV 2 

PPS/DP LAC. 

SRV 2 is e11ubl0d by SRV 2 TAAJ\SFUR, 

Commai:d 

TR.tu\JSrER. * 

Enable 1 

gh•en 1. 8 :L O, 2 secor1ds SRV 2 

f.lCS TER!l-11?\ATT ON ENABLE 1 l) 

Function: This comrnand enahles the SRV 1 AD.fl-1 i;:,onmand from the 

mm,;,mml 

GE RESD. 

3. 12-SO--

ynp ettiir c 

-

H11r11l1c via BYEMAN 

(;;mtrol $ysl1'1'f\Crly 

Approved for Release: 2017/02/14 C05097360 

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• 

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T 

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Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017/02/14 C05097360 

T~CRfT 81 f-008- W-C-019842-Rl-

(2) Uurly dri of a1onitored di!:itance!:i 

(3) Lung-term 

Sl-PRG system inakes three direct, noncontact a1ensuren11 .. :onts dista::i.:es 

within the PPS/UP EAC.. The Sl se11soY mea;:::_urcs the distnnce bet1-:een t 

floss corrector and d lens assemb (RCFL;\) housing 

and the +Y, -Y mean (0-ve:rage) position of the A- s on the 

insj de s j cs assembly (COA) .. 

two PRC sensors measure the distance frorn the +Y and -Y walls of the 

t01'W8td ( end of RCPLA to the 9 platen plvot wh cnn be related to the optical ·1: distance [ ·-X end of the RCPLA to ane) . 

J\leasu1·ements arc made to approximutely :t6 .. 25 inches Crom the PPS/OP 

L1\C optit:a1 cente1·11ne. S.1nce tt.·.ro meA:surements a:re made, both tilt and 

displaz:ement can be sensed. 

The 

(P1'1 and 

ein operates under control of 

r :::uppl by the 

command proce!:i!:ior. Nomi11ul 24.Smonltor o.n<l control 

are conditioned internally. The electrical tion of the 

!:item con be a::y one of three modes :>electable command. 

r 

(1) Of±' 

(2) Read 

( 3) Calibrate ("heal th check") 

stunce fiiurCS", reference Part 3, Section 3. 

3,17 T~ECl!ET G 

Approved for Release: 2017/02/14 C05097360 

Hardlf 11L'l BYfJ4AN 

C6nt·n:I :,y::,lwo Ord l 

• 

• 

• 

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I 

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RET 

I 

T 

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R 

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R 

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1 '1 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017/02/14 C05097360 

T~RET Bl F-OOB- h'-C-019842-Rl-80 

l'he sensor str11cti1rc is a nionolit}:-ic, nearly cubic tnvar s11pport fYame within v.;hich (or upon whic}i) aTc niuunt 

(!) The inductive sensor 

(2) s~ de gearh0ad motor 

( 3) 

f ·1) 

A health check slide arid rctaj ng components 

health sllJe d ve 1even: ;:;nd cams 

(S) i'licruswi Leh cs to control r:totor stat11s 

The sensor attaches to the RCFLA at throe r1ts using pedestal stand0 which nre integral to the frame. 

Vis11a l and seal c uf t!tc as ly a:ro shuwn S. J ?l ·.), Both 

internal components and exterioY configtrration are i l l11strate<l. 

1:;. /f. 2 PRC Sensor t<1011nting 

g1rre 3, 1'.1-!J 11111st1'ates the PRC sensoT mo11nting locations (and the Sl 

sensor Jocation) a:, well as the nodulato:r/demod11lato:r 11nits and the sensoT 

encoder and css 11nil. ·rhc internal rnounting of the PkG sensors with 

to th0 wall is shown in 

so1·s aTB held hy· sc:rews, with an epc,xy mateTial appl to th(• screws to 

effect both locking an<l hc:rnictic scaling. 1\ total of five support 

are involved. three ;:;s shown in f.i ?i.1:\-·i and two applied as additionri.1 

support for the n1otor which wo11l<l otherwise be cantllevered. 

PRG larects arc t:a:rx ic<l hy· the 9 fran1e asse111bly of the dual DtE:n 

came-ra, The 

lnVUr' Ce Fi 

.:ire Invar rods which terminate in 0.6-inch dJameter 

5,1 6), Disc 

Tr!T 

H<anol0 v'a 6YEMAN 

Cortn~I S;~t1,1' (}'·iv 

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T 

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Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017/02/14 C05097360 

..---1'a:rget 

~G BIF-008- 0 842-Rl-80 

Pivoting 

Attuchn1ent Point 

• 

• 

osr· • 

sensor axe;,; al the i lion, !\tot 1 on of fo11ows an arc 

as the pivot frame is adj11ste<l al>cn1t its vot point, with the result that 

the disr, faces do not remain a,r to the sensor axes. Since tl:e 

arc inount at unequal Lances fron1 t point, 

amuunt tilt va:ries from one to the other and yJelds a different responsc {otttput versus separation) for each sensor. 

The Sl teri;er which r:e1ded to the S! :rod 1,", a po1ished Tnvar disc, simitar to tht> PRG discs. !JnJike the PRC the Sl 

nnrnendiculor to the sensor s as t snnaration changes. 

13.6 Health Check Slide 

Each gage assembly i;; equipped with a movable Jnvar tax-cc\t w11i;:h ;:an he 

placed a fjxcd and rcpcatabl 10 distance from the sensor to establish a ren1ctisu:rement. 

magnet de motor :1s a 

viously in 3.13-3. 

on whi l t 1novef.. 

s! ven by a. gear-re11uced 1lE'1'llla11er1t 

al can1 and gear arrangement as showri preLeaf ngs hold slide in contact with the 

e train functions in the 1 oNing nlanner. 

~ 

Z.13-12 

G 

l{aro1t v> a BY At{ 

{):.r\rol Orly 

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B 

1 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017/02/14 C05097360 

T~CRET 

Bl F-008- W-C-01984_2-Rl_:BO 

connects +S-volt motor control frunt the SLPE unit 

to nne or tl1e two sv;i tches on the t11c 111otor 

reaches that state, a can1 the pow 

tltc motor ls ::t Upon rommandJ 

sv.-i tch,; removJ ng contro 1 power, 

0y,pcrni tc state, power 1 s 

transferred to the sct:ond 1nicroswitth, whith ls clos the motor js 

set in mot ion. As the motor turns, the open swJ tc-h c 1 oSfL'>. However, 

crotrctlve odes ia the 1lne cu1'rent fyom b+d ng coup led 

through this switch. When the new conunandcd :>tatc rruc:hoJ, t tch 

rccviv1ng control power ls so t!1u motion is lted. TotDl time to 

drive 5 j j one Jtion t:o the othior :is approximately 32 

01tce motion hes begu:11 1 comman<l:lng the oppo::;J te stDte b~ 

wJ1l ha the drive, t.1otion can be r1!~11med hy re-

'ing the original command. If an opposite r:onnaa.r1d g'ivcn er 

swit are closed, tl:e system ;,;j 11 so.tis the or:lginal r:ommDnd nn<l 

f'Ontinue drlving t.o sriri~ the _;;econd command, 

1\ctual vc power for the motors is derived 

Motor cont.rol potvcr from the 111icrostf:i tchcs 

24.5-volt unrcgul 

ocuvucit:s opt,,'!cul iso1a24.Svolt power to the 1notor through a 

t 

ltcr nctv;rork which controls vol 

13.8 

USC. As a 

13.8.l 

of the Sl-PRG involves i n-factotv, 1 au11ch , and on-orhit 

of in-factory 11se, baselines for orb l oncr·ation arc cstubUse 

For in-fautorv testing, systcnr output is availahlc in two fo·nns: the encoded 

output wh is c.0ndlt1oneo to trru input 

Approved for Release: 2017/02/14 C05097360 

:rcmcrtts (D-5 and 

ttanlil e vi a BY EM AN 

contrtt! Sy$lem On!y 

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T~ET BIF-008- W-C-019842~Rl-80 

13.8.3 On-Orbit Use 

launch orbit cction, Sl-PRG power is tu:rned on four seconds 

ef1:er ECS clock start~ which occurs at SFCO. Sl-PRG on 

384,8 seconds, i1roviding 204.8 11sab 1 e data, 

On-orbit, the Sl-PRG power is tt.rrned on and in ion with the 

FOCUS !CS POWER ON/OFF conunand. can be from 

the Sl-PRG system while l focus on execution of Sl-PRG 

OlSABLE. The disable eppl $ only once and is by tl1e next 

FOCUS ELECTROXICS POWER ON command. 

Sl-PRG calibrate n1ode re<1uilrc1s Sl-PRG power to be on. Execution 

Sl-PRG CALIBRATE th ch<1ck slide in the calrn1rate 

po1,111on. Calibration ends in conjunction wJth the sensor calibrate 

and the s is withdrawn the sc11sor 

Planned on-orbit is va,rinble fl i to-flight and even wi 

given f1ight as conditions desc1riy1tion 

provided here. However, it is 

on•?racted as soon as 

sh:ctt, and 

pr<,ctica1 

that the sensor systen\ will be 

er launch to monitor ony through-Jat:nch 

sensor systcin ibrations 11 n1ost likely be performed several times 

on. 

the miss to 

Vdllntl .i11 the 

thcr1 be calibrated as 

long~ter:m d 

A priinc 

warm-up 

shown that 

od to stabilize outp11t 

a 180-scc;on;l wtt1"ll1-Up time is 

tern can 

reiva'lnclcr of the mission to track 

neces1n1y £or a s1gni£icant 

eve:ry normal use . 

Hardlfv<a 

Cord nil 

EMAN 

~ET Oniy 

Approved for Release: 2017/02/14 C05097360 

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• F1fteer1 minutes (900 seconds) min:imum w:il1 

Sl-PRG cal 

13. 9 Sl-

• A summary the sensor in lo 3.1 l. 

• 

• 

• 

• 3.13-21 

~ET 

Approved for Release: 2017/02/14 C05097360 

Blf-008-

be used 

ion 

-019842-RT-80 

to 

is 

Hanctie v111 BY AH 

Cortro\ $y5t~~ Or\y 
~ 

"' N ' 

N 

TMP 

5561 

tt,;mdle via BYEMAN 

~ 

Approved for Release: 2017/02/14 C05097360 

TTTLE 

Sl Outp11t 

3,13-1 

Sl-PRG EXPEH.T~1ENTAL SYSTb\1 TNS'J'RID<1EN'fAT10N SUR1bIARY 

DESCRIP'l'ION 

An inductive pro.'Llmity detector rriounte<l on 

the 1 oweT ( - Z) portion of the RCFLA housing 

monitors ion hetween the detector 

ond an Invar target on the Sl rod. The rod 

extenrls from ueo.r the detector to a truss 

assentbly connected to the A- ~'Df?I>Ort 

points or the COI\. 

'rhe distO!lCc 1nea~_:ured by the Sl sen$Or' is 

a .o;egme11t of the optical distance, that .L'..l, 

the distance fron~ the +X sUrface of the fi1'st 

RCi'LA lens element to thE' front surface of the 

pr i raary nri rror. Output of the sensor i :; p:t'oces by the sensor encoder :and proces:3ing 

modu'lc to conform to the 0-5 volt telemetry 

POWER 

±15 vdc 

ronge nnd is linear fro1n -7,42 x 10-3 i (0.0 

vol to -f7 .112 x 10-3 inches (S.O voll 

Uistanccs q11oted are i:ncasured witi1 re:;pcct to 

the nomi no 1 it I on. Positive changes ind icate target motion in the +X direction 

separartion in('..ren:des). The telemetry output at no1ninal is 2.50 volts. 

For the calibrat:ion or nhea1th check" nrode 

in which a slide i~; 11ositioned a 

distunce fro111 the sensor, the output 

Ls nominally 1.80 volts, Changes from th 

are linear and fol low the :;ame 

verstis volts 0ut1>ut slope ns 

the normal operational mode. 

μrt)dtrced in 

""'j s,,,,., '''" • • 

-pproved for Release: 2017/02/14 C05097360 • ~ET. 
Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
!MP 

5007 

Approved for Release: 2017/02/14 C05097360 

Bl F-008- W-C-O 2-Rl-80 

TABLE 3.13-1 (CONT'D) 

Tll'LL 

5 Focus Drive 

5 t.1inW5!1>TC'P 

Sl-PRG Cal 

9 Pocus Drive Enable/Inhibit, 

9 1'linus/ , g Plus/Stop, 

Sl-PIZG uic,avl!?/Enablc 

Sl-Pl{G Power Monitor 

OLSCRIPT!ON 

La rel ayn ing the input 

relays of the command 1moc1ossor monitor the 

rect'ipt of commands from the satellite control sect ;;ind O.Ov or 5,0v 

to an ed circuit D/A converter. 

four relays and one 4-bit D/_i\ converter 

form I~4P. Output occurs irt su:rcc:n 

discrete frou1 0.2Sv to 4, 7 

in 0. 3v 

Bit 

!tit 

Bit 

Bit 

Simi Jar 

increments, 

(LSB)' 

2 = 

3 = 

4 (\\1SR) **~' 

tc TMP 5007: 

S rot:ns !J:ri ve Enab 

5 Mi 

5 Plus/Stop 

Sl-PRG Cal On/Off 

ahiblt 

Bit 1 (LSD) -- 9 Focus Drive 

9 Minus/Stop 

9 Plus/Stop 

Enublr:/lnhlblt 

B1l 2 = 

Bit 3 = 

Bit ~ (MSO) 31-PRG Olsabl P/ ICD<>IDlc 

A two-resistor voltage divider network across 

the S1-PRG fef:d in Pfl-1 C n1onitors 

tlte voltflgc output 1 The oi.xtptJt is converted in the d1 ta1 tclcrrtetry unit to y 

a b s (on/off): 

11 0n ., 

0 i" "" On 

B gni Bit 

**MSB - l<fost Significant Bit 

t1111111le v1d BYE.MAH 

Cc<.S,,lm On!. • • 

Approved for Release: 2017/02/14 C05097360 • 

POWER 

+S/±15 vdc 

Self 
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B 

1 

1 

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B 

. 1 

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PART 4 - DU!It;N; t-1ANUFACTURE, TEST A.t\D F1ELD SUPPORT 

1.0 DESIGN 

design of 0 Payload l :Platen Extended Altitude 

Capability EAC] the latest in nn evolutio11ary 

which, the design nf Flight r.-1odcl 1. 1'hi s vehicle, the f)rst nf 

the Gn.1nb:'i t ' was laun 011 n sev sion 1967, 

Hardwure impro"itements since then hnve resulted in imi)roved ground resolution, 

extended orh:l t 1 i fetime, and 

1'hc ettccti vo on F!\1 1 s 4 8 t11rough 54 were di roe ted toward an increase in 

the CμJ''"'"'"' "l to of tn'.rgoet 

rcqui ren!G"!lts. This 

to a w:i 

flexibil is the result 

nn<l 

the i11clusio11 

provides a 

tl:e 

dual platen car.1cra whlch, with ropr.i.o:tc filn1 loads, fi ltn 

for The added rements from the cxtcn<icd 

altitude necessitated 'further changes wl1:ich are 

54. 

speed resul 

to the EAC 

slant ranges, 

Other irapruvemcnt;; in the a:rca.s of 

and 

for the 

decision 

1.1 

A 

45 miss ion. 1'hese irr;pX'O\'enrerrts 

tlie Air Force to plan mission: of uμ to 

e es11abl1 for F~l 1 s 48 thror1gh 

to implement 

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lm ive 

pyrot,,otm1c event 

i11forn;ation return 

have a1so contributed to the 

60-<ley duration . 

54 was that 

dual caraera and 

ttandlt: via BY£MAN 

J';ilrd:rv1 Syttr<m O"\y 
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~RET G 

81 F-008- W-C-019842-RI-80 

such changes as directed by tl1e .i\ir rorce. "J'hese direct 

su:wn:'Ti.zcd in tl1e following parDRH1phs 

l.1.1 Frequency Phase Lock Loop (FPLL) Dr 

"l11is drive improves film utilization 

shut-down~ thereby .reducing film usage at t11e beg:lnning and end 

ee Part S, Section 2.) 

l. 1.2 \lariable Width S1 it 

start-up 

of u 

are 

and 

The sixteen discrete posi ans (a minimum of 12 is required by contract) provide the 

ull 

c.apacbll i ty to 1)roper 1 y expose a broader range of film unde:r 

co11di t ions of target il ltnnina tion. The des :l gn chosen (see 

Part 3, Section 2) eliminates tl1e slit-c 

1.1. 3 lmp.roved Focus Detect ion 

This improven:ent is designed to increase si 

variability. Furthermore 1 the in1proved s 

le rate, and tl1 tl1e 

failure mode. 

-to-noise ratio, reducing data 

-to-noise ratio, :in increa.'\ed 

lter software Part 3, 

Section 9) are expected to inc.:rease the number of le focus estimates, 

l. J.4 Replacement of Separation Control 1er .and 

Initiator Electronics Unit (1RU} 

Electronlc.s with 

'l'he funct1 ons of separation controller and sw1tchover elentronic.s ore 

formed by a new 11ni t, the electronics unit (lEU). Improven1er,ts are 

realized througl1 separate comnrundlng SRV 

technic devices, additional instrrur.entation 

end todundlem;y of 

4. l-2 

direct commanding of pyrofo;r indicat command receipt 

events. 

T~T _Ji__ 

ttaridle v1 a BYEMAN 

OJrit;ol Sy~trm o~:; 

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1.LS Rc<loslgnc<l Comrna11d Processor 

The added re 1iabi11 ty redundant co1mnand suurccs 111 the SCS is extended fu:rtht1r 

by co11tinuing the redundancy through the PPS/DP coinrnand processor. 

l. 2 

Certain design changes 1>.'ere necessitated by the Extended A1titude Capability 

:rcquireu1ent s. c design are summarized in the folloh'ing paragraphs 

and are treated cxt0ns ely in the appropriate subsect 

volumes. 

1. 2. 1 Frequency e Lock Loop (FPLL) Drive 

The availal.ile film drive eccl range has been expanded to accorruno<late the lower 

speeds required for operation at alt udes up tu 470 nmi.. ·rhe "surveillance" 

or 1ow-modc range is frorn 3.37 in,/sec to 23.6 in./sec; while the 11searcl111 or 

is fron; 0,8425 in./sec to 23,6 ln,/sec. The ap1)roach (See 

Part Section 2.5.3) utilizes a conutrandable high/lo..: "switchn, Rcdu11dant means 

arc provided fox switching into and out the high altltude range. 

l.2.2 Focus Detection Systen1 

The wide 1·ange of s1ant ranges v.·hicll must be accomodlilted Dy the EAC PPS necessitates changes in the reticle a11<l e filter Part 3, 

Section 6.0) 

l. 2. 3 Dual Platen Camera 

Required in the dual :olaten camera include chas1ges to the FPLL encoder. 

the addition of a scco11<l sn1car slit in tl1e Priniary Recording em (PRS) and 

the addition of a smear slit to the Secondary Recording System (SRS) . 

4.1·3 

T~T 

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G 

ttardl~ Vld SYEMAN 

Cortrol System Only 
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~ET 

Tl1e encocler oh:mgo i:riv<in•cs in<:or-poration a hi rturnber of (See 

Part 3, ion 2,) 

Tl1e second sn1ear slit Recardi11g Syste-m (PRS) is dcs1g1wo to 

enst1.re an adequate number of smear o dual-11:odo 

IS11Tvc•.illancc arid Sea ntission. Part 1 1 Sectiort 4.5,) 

Chan ha'\te been to the ad,lod commands red to shift from 

the conventional to the Included are conu:na?id ow,pi:ts to the: 

SABLE tho SRC Cl'.(Clllt) , FOCUS Det on 

and filter charactoristlcs), and FPLLE encoUer ). 

ly, a further ohor1go, not necessit.:1tod by , but rcque:>ted by the 

Air Force• is the• CAMERA AlJTO?iATlC Off (CAO) feature The CAO is t1esi to 

vi i·odwvdimcy to CA.11,lERA Of.F fu11ctio11s whe11 one half the ECS has bee1t 

disabled. ng half of ECS 

powor~.sa•vii1g technique. 

I. 3 Items 

As the design progre,;sE:d, it became apparent that 

ohani:os would have ta maJe. These 

obsolescence a11d those lrn:or 0 ocal:od to 

re<lUl:ds:ncy, Cl1anges and improvements l111ve al.:«o 

4.1~4 

TQP 6!Cl!T - Approved for Release: 2017/02/14 C05097360 

consi<l•,rr>tion as a 

aortni onal, relative 

necesr1ta1:0<1 

through ad<led 

in test 

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2.0 ACT 

rel 11 i has hccn a or objective the exj stence nf 

ovvrDll DlF-008 Rel ll Frog rum 

gt1red to meet the intent the dvllncs established 

Ketiability 

The 

for 

evo1t:tinn 

!:>tems nn<l Equi 

7. 

>llL-STD~ 7G3A, 

Prod1:ct1ion) . 

ssJon (F1 :JO) 

lntens:tve re] Jabil i efforts to a:ssuYe he1r<li,;arc cornpatible 

with the associated increases in mission rcquTrerrwrtt~:;. ~l:rx1mized onorbit re1iabili 

an cxtt'ns.i.vc qual 

has been achi 

cation nronn1m, an<l thorough testJng nt mult 

y levels . 

rel iabj 11 into the 9 x 5 hoz<lware 

rnncer1t1ial phases. 'lcchniqucs ond 

been a major since 

earliest i l cs r lff'1Xrntiorng 

rcliabili 0rrninaiio11 uf: types of 

dc;,rce of rcdund the as ly 1 evel at which redund shou 1 d be 

implemented, and, in many cnses, how to best use exist hard'wa11c where 

rcdcs was not practii:.:al or not purmitte<l. 

ReliabJlit 

of the tors in the development of high rc1iabl1 i haTdwarc is 

compatible with thjs goal, This is hest accumpl 

ing fo1·ma! design reviews •1.rhich cxai:iinc and critique the 

all 

desi 

l 

1'hc rcvieh' items incl 

( S.lntpl 

the dt:ve1op;nor1t 

but al·c not 1 imi t 

1. 2- l 

Approved for Release: 2017/02/14 C05097360 

p·haSf' 

to: 

implcmu11t~ 

s:ign in 

na-.di• v•d BYEMAN 

1);wt•o1 Q"liv 
Approved for Release: 2017/02/14 C05097360 

~T 8J F-008- W-~:-019842-Rl-80 

(bl Stan<lardiic<l pscrt;s ,: c::m1po:ocnts/rnn tcrial s 

Te1iabi1 

( c) bes le pc1·fo:rmancc rc:1uiru:mcrtts 

( d) Interface c0mpatibil (piece part~ component <:tnd subsyste1n) 

Design le cxtTC!Jlt'S 

( f) 1\<lequute SB y ina demonstrated by test and worst cnsc 

ana1 s 

Recognitio11 of test requiren1ents 

of the ho rd:rnre tticularly in re<lun<lnnt ateos 

( :l) t\dequ:;,cy redundancies - at aJ J 

(j) Recognitinr, and identi 

an<l 

( k) :nm,m:z:nlon of slnglc poi1tt 

cf nl 1 majo1· fai Ju1·e modes 

lure modes. 

c ite:m:::; nrc generally examined at the compnnent (box) 1eve1, Howeve1·, 

compon€'11t may empJ uy ce-part redundt111cy a11<l ltigh re il cirand/01: t Redundancy is also extend.;d to the 

levt>J 

2.2 Reliabii 

In to i1111strate reliabi merits of the rt' PPS/DP ' it 

1 s nee cs sary to consider the 

and trcnt each one 

as being c1.nnp0sed of various subsysterns 

·ren suhi;ystems have beeTl selected for discuss ion and b 1 ock m0de 1 i 1 lustrDt ion. No at tc1upt 

an 

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been made to determine 

ifJn::lf via BYEMAN 

(nr,tff:d Syst'*rn C'l!y 

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for Release: 2017102/14 C05097360 
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T~RET Bl f-008- W-C-019842-RJ-80 

rather t11an t 

for each bit are 

two bits uti1iz foT the stereo 

symmetrical foe rel lity 

itlon. The 11 $ and 0 1 s 

ling pnrpo:ses so both 

states arc not shown. 

Ins trun1enta ti on 

fj ~.2-4, 4.2-5 and 4.2-6 illustrate the major ions of the 

instrumentation subsystem, The focus sensor, S 1-PRG sensors and tl1e film 

path transducer are all considered a of this suhsvsterr. 

As s11own in Figure 4. 2-4, the instrumentation suhsys,tem 1 s desi 

pulse code modulated telemetry ( slave unit which two totally 

rcdcmuont H (PO.t #1 PCJl-1 is >I 

tt2u) . Both of 

unit ( MDTU) 

es conununicute w h the master 

address and reply• 1 ines. 

aci1nal tele1ne11rv 

si (not both) 

can be ON by any one corrunands: the usual ECS A 

or B (lOV*"') a variable word comnuand the lilCS or a 

real time command also frorn th€ ~\CS. In addition to the PClll t1nit, 

set of PC&-1 also en,"2111A;s the S-vo1t J ator 

in the PM and 1vhich are util 1 

the :t1Svolt converter (both by rnost 

t11e inst rumen tat ion nts (sensors,, txnnsdueer'S switches, etc,) throughout tile PPS/DP EAC. 

monitoring instrumentation points which are of primary erest is uee,om11lJ,shed emp1oyi. both po\1er sources vo1ts and 

±15 volt applied to two similar sensing units (sensors, transdluc e1•s, sv;i tches, etc.), These units are locat es ru:;etional close to 

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TQJ! &EtfiT G 

Bl f-OOo· W-C-019842-Rl-8·~· 

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other as possible. The nts arid fucno.tions to be mcni tored have bee11 selected 

and in<itrum<mtod such a ma1n1er power ::;:ourl:e would provide e • 

in format i 011 and <l:i ugnost 1 cs to monitor the health of PPS/DP £1\C <luring operatio11. 

t:igure 4,2-4 also illustrates the non-redtnvJanl (and noacrlti use the lm 

path press11re 1'hi s 

l}oth sides of the PCM unit. 

a self~ contained inst.rwnent is n1onitored by • 

4. 2-$ shows the rellabil model of t!1e focus sensor sulisvstein. "l'wo oonmoands 

are avai le to activate the sensor whi1e comreands (not shown) are for 

"l'hc sc11::;:or cal 1brw.to circuitry is both activated and, turne-d o by 

four i ble conanonds. l~ular subsvstom is oo'1gnett with 

on disac1rng 1•a:ther enabling as can be seen by the 

[tatner t llcl) and the two 

r swit 

ea;phasi::;: 

$ 

tt1rn-off. For 

the EAC confj gu'.ratcjon, the High/Low Altitude functlo11 has 

detection electronics and the calibration has been 

added 'lo the 

exr,endeO capahll-· 

itics. The High/Low Altit11de commartd incorucnct<lS a ttnique Teli 1 scheme 

ln thttt ls a:.::,,;onrpll,!:)ht+d by employ 01ther dcoodor A or decoder B 

commands not simultaneously} wh:! ch rest1lts :in nclclitional fallut·e workfocus sensor information is 

Fi lificd model of the Sl-PRG 

uses the same proces turn-011 a::: 

to both sides of PCf,1 imi t 

for 

The Sl-PRG hardware 

foc11s ::;:c11sor, 'fhere 

are six p·osslble co1::anands for turr1-off (four described nr·ev·iously for sensor 

OFF two as Sl-PRG tui•cti on hos re<lunJnnt 1ON 1 

the sensor calibrate, can i1ti lize 

commru1d:s. 11:e Sl-PRG be rioncritical is, 

more emphasis un turn-off than, on turn-on. lnformot 

cessed PQ.1 unit. 

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sible 1 0FF' 

designe<:J t.'ith 

Hardlt v1il BYEMAM 

(;ol'ltrul Sy:;.t!'nt Onl ~ 

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BIF 

the first bits, 1\11 of these commands are received redundantly from 

the ECS. 'I'he FD+ and OP concrnands enable the SRC drive circuitry and "ermjt 

SRC lnotor to ust 

it us dictated by tht'l 

Dtte to cu1tsequences of tl1e 

until tl1e encoder 

bits. 

ible l 

sat cs the des 

niodo$ t empha$is ls on 

ub1 ing tl1e ~.ubsystem. T11e drive c is •d (24. Sv power ri;ntov0d) 

by an;y of' the foll conu1i.1nds: fl lm OFF (FD-) ; SRC 

DIS,\llLE; redu11dant 13V command word impl 5 OT 9 OP OFf 

sing1y; minimal 5 and 9 OP OFF received singly. 

2. 2' 7 Subsicstems 

lloth the 9 und S subsystems are ider1tical 

snc subsystems. are totally 

modeling 

from one 

and, as in the NP/\ 

The VEM ntod el Cle1$ely 

resembles t11c 

st:raigl1tforward and classical u~, 

NPA model and is considered one of the most 

of re<lundm1cy in the PPS/DP EAC systo111. 

Figure 4. 2-10 i 11ustrates the features of symmetri cn 1 and cl ass i ca 1 redundancy 

applied to the VE~l 

pr•oc1,s1,ed reJu11dantly. 

Redundant enable/inhibit commands are received and 

se COHIJH!UidS ly/rvrnove urtswitcJ1.cd power to th0 

and motor drive circuitry an<l are steered by the redundant se VEJY1 S1de A/Side B 

command. 1'he position commands (bi (lre 

The .E~1 1 and motor dr circuitry fo1' botl1 si<l<: A a11d s L\ are identical . 

Both s provide n1otor d"t·ive which is ORed at the motor. A dt1a1 encoder 

sttppl Jes lndcpemclertt position feedback for cacli 

2.2.8 9 filnt Handling 

A r0elundartcy block diagram lnr handl 

4.2-11. There ar~ two commands reql1i red to 

4.2-18 

T~i 

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cm is shuwr1 in figure 

ouer·ate the 9 fi ln1 hand 1 i.ng 

H11ndlt 111a BYE.MAN 

Cortro! Syst~~ o~ly 

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tne setift c -

Bl f-008- ,~::, 19842-Rl-80 

i\ecci of the ant tak lNlllBl'r t rc:sulLs lTI D 

sw1tch contact c losurc 1n Lhc c unit. A11 inte1'nal 

c SW loco:ted J n l;L Jj el ;;;ct cs ex ~~cutes the 

ly toop+>r FUl.L and E~lPTY 1o.r;ic sv.•i tchcs, 1ocatcd in the ly unil, 

will th<' film takc-u:p Lio11 in lhc absonr:e 

t,his command, 

ing trrake OX/OFf co;rn11nnd is th cs 

the command 

the rcl1abili 

T!loni tor and control uni ts. 'fo 'Increase 

cf stern, a 1-safc igJl ttrro the suptJly 

rk brake c:ircuilry has been pruv ed, In event th'.Jl the corK1nc 

cannot be i. n .S supply 

unit will disable this runction with the lication of S OP power . 

fhe 

which 

lm ndl 

des a l c1rgc degree tnnc.tionn l 

er of s inglc 

l 

'.:',2.10 Thermal Unv.i..ronment Control stt:rn 

mode 

The t:!1ermn1 environment or the PPS/DP EAC is control led 

onc1ution cJ rcui 

xhilc su;>7Jlying nn 

iterns: a system, p<1ttern, and door opf'Tation. 

c:m anG Paint Psttcrns. The heater cm aud t 

in df't:'l11 in Part 3, Section¢ of this durun:ent, 

"fhcre arc, f'vcr, rcJLabilily cuns tions which 

into the thermal control s The 1ng system is a scri cs of 

"branch" swLtches 8 l ;1 number of heater contTollcrs that in 

turn thcrrno:>tnt1Cal ly control po\\ er to 

4.2-23 

TQP SECRt'T 

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ha1dl r vi a BY AH 

0Jritr·01 :;yst,:rr 0·:1 y 
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B 

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2 .3.2 

2.3.3 

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~..L 

Purpose 

(a) To veri the l the uncl1u11ged. new or 

signi ly modified port of the PPSfDP LAC 

design to meet ional and envir0111nc11tal rements, 

\\hen subjected to extremes of environmental conditions. 

(b) 1'o discover 

tcctcd 

failure modes not pn:viously 

(c) 

(d) 

(e) 

Quali 

·ro idc11t ify 

PPS/DP BAC, 

the 9 x .S 

unchanged areas. 

eractions between portions 

espe<:isclly in those 

1nust 

areas 

hv:r1nony 

adequacy of the munufucturing, 

occ:ep•ta:nce test JffOC<:d1ircs and support eq<>if>mcnt 

To vorifv the ins1>ection 

and 

To the overall reliabil by 

:Culfillme11t of the ahovc. 

cation Testing 

\<uu lification testing is designed to demonst:rate that hardware, 

of px·o:lu,,tion. can meet its specified functional rrrou.ircrrcercts during 

exposure to signated extrenies of e11viro1'1nn:nts. 1'he COflSl>!S 

of a of tests on the major elements a110 compo11ents of the PPS/DP EAC 

(9 x SJ en1. The tests si1nul0-te types of environments encountered by the 

hnrdware and include verifit.:ation of ficd at mul USS>JIHbly 

levels. 

2.3.3.l Qualification Test Criteria, The test criteria, test levels 

μurameters involved are based on t11e requirenients origi11atir1g froni th.e General 

i11 BTF-008 sp<>Crficntion 1402-320 

{Environment al Design Criteria) an<l de 1 i neated 

1402-558 (Qualificatio11/Confidence Test Plan). 

detail in BIF-008 

1·he ronmentnl test levels to 

which t11e hardware arc subjected arc gt-'11ora11y more severe th:m maximurn antic1putc>o 

4.2-28 Tr-ET 

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Centro! st0~ o~ly 

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2.3.3.2 

test 

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levels for the following reasons: 

(a) TT~oa~~ii~~:~te for inaccu:i:ncies in 

o c11vironme11tal levels. 

knnw1 of a(.tUal 

(bl off:>et the fact that 

simultaneously 

certain environments are enco11ntere<l 

ac·tuiil use, but arc appl 

<luring testing . 

(c} To e normal variations vi dual 

the same design. 

(d) 1'o provide additior1al confidc!1ce in the abil of the 9 x S 

hardware to levels. 

(ej To pa1:tially statls ti cal l imi tat.ions :;mall 

sample 5jze. 

(f) 1"o verify tho:t a nw:no11 j5 Jn 

ro acco1111t the fact that n given piece of harJ4-a:re muy 

a test excessively 2r<1a1.e1· than normal . 

Test Hardware. Qualu:icn:cion test hardwa:re 

al 1 the normal fabricatio11, 

an<l 

buildup~ as:;cmhly, ha11dl 

col fl 

which hos 

$ c11vironment.s, 

be subject 

hardware is de<licnteJ to r1ualificnt testing use only rind is not 

flight. 

2. 3.4 Dem on st r :a va<l 11u11un •Cat ion 

Table 4 . l linccabes the demonstrat uf major 

eornpcme.nt and n1od1<le. (JJue to evolution both fiambi t Program an<l suhseq11e:ntly nll items <lo not reflect similar levels of ification.) 

The 

not 

test 

reader must he aware 

riecessarily 

method (equj 

2.3.3.1 . (In 

values 'I'able 4.2-1 are values 

s. ·rl:c reasons are contractual, 

D'.l; intentior1al overtest as described 

gc1ao1:nl, art overti:st of 2 

4.2-29 

TOP $''•ti.-C 

-

is enrployed by BIF-008.) 

ttafldl~ 111a BYEMAN 

Cortroi 51~t~m Onl1 

Approved for Release: 2017/02/14 C05097360 
Approved for Release: 2017/02/14 C05097360 

....£.... Bl F-008- -019842-Rl-80 

Notes: 

Key: 

,\bbrev.: 

Hanote via BYEMAH 

1402-320 

!402-320-A 

1402-558 

1402- 2 

--~ .. 

TABLE 4.2-l 

RLL!AB!LlTY 

QUAL!FlCArlON TESTS 

tuviro11mental Design , Qual, & • ·re:;t Levels for s

2 

Envi1'011meT1tal oria for New Des a11d Acceptance 

Quall ion 'fest Requircmcr1ts foT FM-48 thro11gh 54 

Qualificatioa/Co11fideace 'l'est Plan F0-7 

Quall fic:1tloa/Con 'I'ost Plan for LAC Configuration 

1. Tests listed are tests performed duri11g the K, or F0-7 programs or planned/ 

performed fo1· the EAC Con ion. 

2, Additional 

3. Thi:; table 

currently in 

* 

*' 

No Astcrj sk 

# 

(A) 

PRS 

SRS 

CRP Test 

T/A 

DTV 

ECCT 

ficatio11 or requirements arc iled in 1~02-320, 

ects the quali.Cication statt1s and ex;Dected results of certain tests 

progress. 

2 . B Quali. 

K-Quali i ctlti on Test Resu1 ts 

F0-7 Quali ion 'fest Results 

>pccctucation 

F0-7 Qualification Vil1ratlon Test to 

Primary Record Systen1 (9) 

Secondary Record Sys tom 

Acot1stJ c 'l'est Results (ATR) Spcctruin 

Combir1ed Record h Test Includes all film hand 

'I'hermal Altitude 

Developmental Test Vel1icle 

Extended Cycle Con fide11cc 'I' est 

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1 

T 

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positions J20 Th-e i;rnt e1'errti al nri cntati on mounting is 

deternincd from and stereo n1irror surface qtial1ty tcstLnp, to optiiaize 

em c. 

Si th np, the ' the Ross corr0ctor· lens 

clements arc polished; and ac:.:: tcst0J, l·ollow this, the 

anti- .i un minus-blue ltCT coat a:re applJeUi UT!{l the i;lements 

o r·e cut to the 1ar dimensions FnT assembly. 

RCFLA bt1il OCCU1"5 in a vert1ca1 with the ca1 axis 

to the gxavity vector. Lens clement three i:td clement from the +'X end of 

tht' RCFLA) is allg11ed to the ca1ncra 111ount holes 

of tl1e RCFLA hotts 1111d potted in ace, The Te ma in-l ng 1 ens el ernents aye 

ir1stal 1 al1gr10e to lens 'flit~ assembled RCl·LA is 

is re:atly for mount in the COA struct11cc. 

3.2.1,2 Opticol Oμt component mountl 

to the COl\ stTuc::ture b with jnstallotJon of the RCPLA, after whlch the 

stereo 1nirror is mounted (sec I· ure ll.3-4) and some t-i;st performed, Next, 

mlrr·or ond bell ass0mb l$ ins tB 11 1ow1ng the P''O<OB<hO'a 

re 4,3-S, l· lrs t, or1 autocol lima t axicon leveled to 

to the i cal of the third Ross elemcrit to estah 1 i sh the COA 

$, The miTro:r and end bell assomb is tht'!l 11\0llllteJ OTl the COA 

to th0 axis 0stnbl by the ax icon. 

The stereo 1n.i:rroc ls last optical co1nponent a11 gned. As shown in Fl 

'i.3-6, two theodolites, each leveled to gravttv, a:re t1scd to align the stereo 

mirr·or, rst, COA str1Jcture is rolled untiJ r·o 11 ref ffoonco mi T rD r 

on the RCfLA ho11s autocollimatcs the source fro111 tlleodollte nun1bcr one. 

'fhe- second theodolite is aligned pc<'DDHD!Cular to the opt 

Approved for Release: 2017/02/14 C05097360 

1 oxis using an 

Handlt; via BYEMAN 

C00troi Sy:>tcw Only 

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the two PRG sensors arc ustcd to their nvminal 

for with rcspec:t to itc; target and t]ic 

Sf'"11sors pinned in plnc<o, St and PR\~ prcvibrati on bas.cl ine.s arc e.stabli:th 

ror th0sc c0nd it ions, 

After completlon of Sl mount , ond ion testing, th<"' \.OA i.s 

vihrate<l with !l cnrnern mnss s'tmulator installed, and n test<:~d. This i:: 

opticnl testing 

best pholoJ:nmhic 

rforme<l on the C()A, nnd SJ-PEG operational baselines it ion bas el invs arc est li at 

time, The cnmero i.s seieC'.tive!y shJnuned at the mo11nt1ng pads too lmlze 

axial norformzmct<: arid li:::e fi cld performance for the D ,s cm. 

3.2.2 External Structure 

The external structute, !:itTUZ'turtll shell lhB PP-S/DP E1\C c:nns:ists of five rnajor .'1'.0sembllcs: 

(1) 'fh1.• Aft barrel 

f _ Forv;ard burrcl 

( rhc supply r:lectronlcs st:ructurr: ( 

ectoble er (EA) 

tv1anu of structure ls per b;· Lo M1ssilcs arid 

Corapany (LMSC] und1.•r subcontruct to BJF-008. Jn ion, Lf<1SC 

many of ternol n n<l nonstruclural LS 1)$ well 

For the forward barre 1, nonstrnctt1:rn1 co:rn0,,mmts include the hatch 

cjet:tion UHj!'O!!OOt $. f·or 

the SES, the junction box. the film enclosure, c.s.b11ng, e1ectr1cn1 

r.eoteTs, th0rmnl instrumcntai:ion, and olhcr components arc installed L~LSC . 

~ 3-12 

JOP 

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Blf-008- 019842,-HI-80 

formed lo check for any m0;;hanical coupling between lhe CUA an<l external 

struct11:cc, arid the Cot-t -1s coniplcte :1nd 

tion. 

3' 2 ,4 SLM Assembly 

The basic SEM struct1rrf' is f'o:rmed by the SES 1n<tnufaclurcd by LP'.SC. Fig11rc 4.'.)-

12 ill11stratcs the SEM assembly f1ow following completion of Lhe by L\!SC 

Upvn i·ccei al BIF-008 fai::ilitics, the SLS is disasscmbl and insp0cted. fl. 

sticky "f1y 

cnclos1rrc lo 

r" cooti is ;;;pplied to the 1ns surfai::e of the film supply 

any contaminants that come in contnct, nnd any nL"'cess 

wiring mo<lificalion::. urc accc'mc'lishcd in the junction hox and clcct:rical hat'-

fur in:;Lallation 0£ the 

rt'n:airting component;,;, including thP f'llm suppl1t's ar1d f'l+:ctronii:' boxes . 

3.2.4. l Filrn Supply .A.ssen~b1 ics. 'fhf' ~and ;-) ly asscmbl ies, cxc-ludinp, 

iccr mechanism:,, are built at BTF-008 facilities. 

"'lssr'rnb1y or rhe 9 ly begins v-rlth construction of the spoo1 c0re .<in<l JTiv(~ 

assembly, and the fran1c and looper assembly (reference Part :s, Section 2). 

The two arc then cor11bincd tu form t11e bn~;lc 9 supply, Next, the y rolleTs and components are aligned for film t1'acking and tht' completed 

assrmhly tested. ·rnc syllicer mechanism is Jnstallcd and the entire asscrnbly 

test once 1nore pr tv instnl lat ion in the S[~1. 

The ,S supply is ass2mb11"'d :ind a1i.gn0d much like the 9 

1 drlvc is not internul to the core 

ics urc not rPqui 

3.2.'t.2 Electron·Jc Dox 

thus two se 

ly. However, the 

anJ built BlF-008, Those not nianufa,-,tured RTF-OOB includi~ the fol lowi.nr;: 

4 .. 1 19 

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Comprehensive testing coinponents: niajor assemblies, modules and the 

grap·hJc payload sect1or,/clonl platen extended altitude capahi 1 i (P}'S/DP FAC:J 

is perfo1:me<l to assure tl1\it BIF-008 1i11ero.ble hardl{are meets ±ied 

remcnts :re1iabi11 and in-use environment conditions. 

Environmental design and test criteria have beBn ost:abllsheU tlte PPS/DP EAC 

modules, or assemblies and components sr•er:i 1" ic;;tt 1 ons, 

the comp11an1.:o with ch wi 11 result in a high-perfo:rncar,ce nr 

Testing of the camera ics assembly [COA) for optical quaJ nnd 

a.nee from testing of the 1ndjv1 1 opt $ t 0 acceiptnnce 

Les of the contplctcd CO!\.. 

4. 1. 1 Lens and Mirror Compo11ent ·rest 

Optical t:ompone11ts are tested for i ty, proper <lin1ensi<HlS, 

factors Linent Lo eact 1ndividua1 element, These tes:Ls are performed afteY 

the coinpon~nts ttnd at es of assenibly. 

4. 1 '1 "1 Primary Asphere and Stereo 1'11 Yro:r. Acce1>tc,nce testing of tlie pr1-

mary and stereo mirrors 1ncJudes interferc•mc•t1·ic evaJ11at'1on surface qual 

ns well as rncasu:ren;cnts of cctance and the vertex ra<l 

;e1yrriT. s ii <l test empl 

quality of tlte stereo and p:rimary mixrors are show11 in 

{';" of gra:v induced u tort ion on the surface l i ty 

G 

Approved for Release: 2017/02/14 C05097360 

the nrimccrv 

to evaluate 

4.4-1. Tite 

lurge l 

tta0dit v•a BYEMAN 

(00tn:;i $r1t<'" D"i r 
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4 4- On-Back 

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vre1ght mirrors is minimizeo Wy suo,llorting the mirror 011 its back on <:t proy inflated air bag, 111 

equivalent ccr1ter of curvature 

i:s locat 

as11l1eric primary mirror or tl1e test 

sphere the stereo mirror. "!he tKo-element 11ll11 cmnp<msator 

whi the primary 1nirror cunve.rts 

wavefront proJuced by the pr i111ary 

evaluation, The eTror c:ontTi 

to a spherical \vavefront 

on of test 

interand IYUl 1 

arc accur<itely known ar1d are taken into accour1t when evalnati.ng 

the quality of 

ments are first 

p.rin1nry stereo 1nirror;;. 

a ft er the 0 tior1 the 

Surface qua measureg'h 

and atter the mirrors have heen :into their mounts. Dur~ng 

test 1nounted mirrors, the mount;; are counte1•-balanced so that their 

does not :SU qual of opt1C. 

4.1.1.:t Russ Cor".rector <:tTtd l:'ield Le1:s Assembly (RCVLA) Test 

mcrtts 1n1Jd 0 oo RCFLA e-l01nents or, where ate, on 

tiVf' gJ ass 1 es. inc.Jude: sur ority, radii, eJ en1ent thick~ 

ne.s:s, ir1dex of tion,, l dis ' homogenei av.cl bi 

test of the assembled RCFLA incJ measurements of thf' alignment of the elernents, air a:1d le-ah rate. 

4,1,2 Lens /\.ssembly and COI\ 

Ross and COA leveJ t nre performet1 w the caJ oxis ho1'l -

zontnJ and the primary. stereo a11d a11toco1 lim.'1tlng test mirrors SU!'J'OTtEcd on 

ge, TI1e testing in the .iY 11p and -Y up vehicle o:rient,c:itions. 

An autocol ll1natlo11 technique einplm' J •o a 4S-lnch dJ01neter test flttt wsed to 

sin111l 

e best focus posJtion for an object at inrrn,ny 4,4-2 is a 

agram of test match and COA level optlcal 

4.4-3 

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te;:;ting, The ect r tDrgt't, int ramct0r 1 etc.') ls local ut l he 

po focus of the lens. Accordingly, the beam of l t re .. 

fl the surface the j s co I 1 i mated and is cctcd by the 

stcrcD ml rro• to the uutocolllma te::>t at which the beam into 

the lens. Tho tcs t flat to Jy i Dn thv return 

Dur doublc-ptlSS autocollimation process, lens aberration:-; and 

rienced in the s e-pass 

f1 c011di ti on, hbiJ e thv e of t s on wave 

linear~ the modulation produced by the lens is in D- nonlinear 

on. A.ccordi ng doub 1 s resolution met1surements ¢;,tnnot be tigor~ 

ously int ated to s le-pas;,; qual i estimate;,;. A.e. an alternative, 

sampJes of doubro-p"ss 

various 

:into;fEtTC>m<<t:ric wavef1·ont 

to v1·o••lde rigorous 

A unscnption of this t 

n1·ect1ctio11s of optical arid 

que can be found 1 n 

Part ? , Section 1:?, "Optic11J Ann 

Match ng, 

mirror i:, installed in the end bell as.semh1y. The RCFLA 

pTim.:iry 

pri1nary· mirror 

(whicl: canst utc tl:e lvns of the COA) undergo u11 rn-prn,coss Ross test 

which $ 

Ubjcct 

obj vet s: 

Evaluation of thv wavefrontt 

of stereo mirror surface 

t'rrors • 

distortion 

(b) Opt zntion of !\CFLA and primn:ry mirror alignment. 

(c) lt12tlon of Jens 

tilt and eld-cu:r1.rature 

( ond (b) ore Dch via 

s to nee, 

characteristic~ . 

lncd ho th 

Lt'St atticuucs n nJ ave:ru to minin1izt' effect caused by Jistortlon of the 

optical compor1ei1ts due to gravity. '111c contrlbution of the calibrated wnvecront 

4,4-S 7•: 

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~CRET Bi i·-008- h-C-Dl 

error of the a11tocoll:imating test flat 'is :removeJ frorn the Hoss match hdVrfront dt1r1ng intcrferorr:ctri c proccssi An est irr.atc system v.ovd'rrmt 

a11d arc rnadc by addition of the wavefront er1·or:: or the Ross 

match and stereo 1nirror to t11e wavefront. Back-focus and :'ima.grc-p!A.re characteristics B:re assessed thro11gh static, double~ s "white-light" photograr>hl_c, tri-bar resolution testing which is performed or, ax and 01 t the 

ll. 05 degree semi elJ itions. Back-focus und fi curvature are contro11ed by 

COA. Buildup. I\ftcr Ross rnatch test 

mix•ror an<l the prin:ary {ass leJ j n 

the internal structttre. The 

and the RCFLA. 

tl'H; RCfLA, the :,terco 

hell) aTe installed in 

deter111ined at the Ross match level, is tra11sferreJ to the COA. The asscmh1y-aid reference mJ1"1"or PA" and the stereo wJrror are aJi;:ncd to the 

vptical axis of the RCFLA. 

The "En (Roil) reference rr;irror is instal:l ed and measured.~· The e of 

gra.vlty-induccd stritctul"al distortion on systc'r al igr:,rc1ct 

av10t,1gc uf the 

is accounted for 

by sett the alig11mcnt equal to the ty-induc 

placements encountered as the vehicle is :rolled 180 degrees relative to 

r;rav'ity. This technique involves a slmple application of Houkc':.; law to a 

structure which exhibit'., little crcs 

4. I .2 _ 3 COA Test Testing at the CO.<\ level is co111p!ic0:terl by the 

grav -induced distortion of the s11rface of the stereo mirror which 1:-; 

support on e (trunnioi: axis verticaJ 1, und the distortion or the COA 

structur'e. The ot:-edg-e distrrrt1on of the stereo 11rirror is minimized 

by supporting the mirror on test jacks inserted into the side n:ount.s the 

·mirror 1 3/8 inches forward of its ccr.ter of gravity. A 1101:n:inal upward 

of 250 pounds p11sh and pu! 1 i;:; lied at the gr'avity-bottorn and gr.avi op 

ref'"'""'" 111irTor 

alJgnrr:ent, 

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W-C-Ul0842-HJ-S0 

side mounts, respect 

the stereo mirrox nnd re1noves its 

::ction n1lnimizes 

ght from 

lty dist.ot't10D ;,f 

1nterna1 structure . 

During testing, the Cl!A is mounted Jn n cradle and supported ir1 a n:annor 

s·imilar to its mounting in the external struct11Te, 

the ".A.n fran1cs and the rod or "hroomstick" of 

esscrrro1.y which is in turri in a 

gruvi un inte:rnal structur0 tilts eote:rs 

COA is supported 

mary 1nlrror ll 

TI1e in uence o C 

RCFLJ\ rel::itive to 

cnrnpensa.tion force::; arc applied at critical 

the structure and of the to reduce structural lcctions nn<l RCfL1\/ 

nLLrxor al igmoen.t 4. S illustrntes 

COA for t:nc•om11cr1S<1tr1d and compensated cases. 

1\l though vi ortion 

loatl compcnsar1on, wreasurements of 

steteo n1irrn:r ltos be0n minu1ued 

qua 1 'i ty made 1 n xny s i 

throi.:q;h 

tesr 

attitt1de arc in error (dcviat<: from the "ZERO-{;" 

res l gravity~ir1d1tc•sd distortion present in the ."-tereo 

the amot:rrl of 

1 nad 

comp•cosa.ti 011. This residual component of p,ravi induced distortion is caneel the wnvefront lical path <l (OPD) arrays obtflln 

in the +Y ori 0ntriti0ns of e COA 

A s1ml lur avvrag technique Is e1npl to cl tl1e s of residual 

struct11ral orti 011 on on of t pl10 phic 

lane c1ia1·acteristies. A siinpli ng ass Is t these 

meter$ o :re and tely e \'eh'ic1e oriental ion to gr av 

Best focus (BPI') churn cs nre then 

fron1 the averngc results ob ta in tJ1e +Y U]' rind -Y up test att 1 ttJ<1cs. 

Photo-oy,ticu l testing occurs D L 

.SF) in a s (opt 1rncuun1 environment tn mln:i zc the effects 

4,4-7 T P/T 

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thermally-induced air stratification or turbulence in the long air-tc:::;t optical 

assvss1ncnl of optical made at the ful I CO:\ assembly 

level COA vibrut aL tancc l 

s, static, heterod11rc1mc1Lcc optical qual y factor (OQF) and 111uit 

har Tesolution al" 2:J contYrtst are from wa1vei'ro,nt samples cbta 

axially, at the t'.enter the;:, platen position, and at the ±1.05 se111ifield angle itions, il1e rneasnred inmccs of the ma nu tt1red refract l ve 

elements 2re empl 

tions 

mC,CLlJat ion tT1JDS-

's) and resolutio11 values. This permits incorr1or'ati on of 

the spec 

lcn:;. Smenr 

axial- and field-color aberrations to tl1e OQP of the 

's cal cul from e 9 and S film dr 

encodt~r and drive smoothness tests are used to ict dy11an1ic quality 

and 1 inp, re-solution vaJues oft 

Post-vibration te!:it 

111ctcrs requ 

( l) ' 

incl11des a ca! 

flight oun'ations, 

tlvc 

('.(),.\, 

ion of those 

inc 1 

(ErLl 

(2) sett ling time of the ste:rt~o inlrror 

o-optical para-

(z,) ;:;te-rco-.:nlrT01' instru1110ntatlon and line of sight (LOS) 

"!\" and '1BP reference mirTor LCJS 

tTansmi:trunce for 

(6) 51-PRG opcrutlonal bast'-llncs 

ructcrlst s arc asse-ssed vla doubre-pass, static, 

tors 

BPF and i magc 1 ane 

through-focus, tri resolutio11 test axiaJ and 1n the ±1.0S 

semi- cld posltlons. 

onv ironme11ral differences, 

e re-sults a:re usted for test lng/ono'1'DctlonThe camera is se.!ect 

zc Dxial 

y shimm!f'rl to tl1c mounting pads of tl1c RCFLA to optiand equalize field performance for the 9 film drive 

G 

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T~ c 

81 ! -008- l\-C-D10042-RT-SC 

CUA is comm1ttcd to COt-1 and hi 

nsseml:l)' bui ·1nc kincu1atic nature of COA si::pport )n the external 

Lli c learancc at critical point;::;, an<l 

hand! t eln1lnote the necessity of optical test at 

hi levels assemh1y. The st CDA as rrnd test ow dein these paragraphs is shown in Figure '1.4-.S, 

E ricol ·rest 

"Component" is a terru used to denote a hlacK hox ro thnn ;,1 

ponent test in$ with 

of wi rei rt111s functional 

tests des 

ooerotlon at 

to demonstrate :integ·· 

so,tc•cte<l points ln the assentbly/ 

ht1i ldttp 5 is or1 electrical ho·ar'ds, n10<lule s, 

motors, encc•dc,,·s, potent :ior\eters and hox subassenrblJ es, object of inprocess testing ls to pe1·furn~ co,ccKs 

and as::;emh1y error::; at the earliest 

u n1inin1u1a test cornplexi 

tu veri operati0n ur dete(',t part defects 

prno>ical point in assembly cycle with 

4. 2' l .J\cceptance 'resting 

test is c-,onducted on all assemhled con1ponents t1ti1izing either 

ciallzed tc:st 

4-6. These tc:ts veri that 

the oppropr1ate draw 

electro-mechanic:ul 

ci fica t 

icBl 

4. 

oarameters coniply 

lb ration 

data ls ohtained 

A typjcal 

those not avaJ 1 able :in highcr-lev01 testing. 

test flow is as lows: 

( l ) In-process te 

( Tnst11 at ion re;:; istance and cont:l nui ty 

( E Jcal ical functional 

Approved for Release: 2017/02/14 C05097360 

tests 

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rtarc1t. ,.,., BYEMA.lt 

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Approved for Release: 2017 /02/14 C05097360 

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for Release: 2017102/14 C05097360 
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for Release: 2017/02/14 C05097360 ___________ _ 
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• 

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Approved for Release: 2017/02/14 C05097360 

~ RI F-008- _1\-C-019842-H l Bl: 

is niodl od us nocu.ssary* and tested SE~'[ l2vel test th0n starts, be1<.ith electrical cuniinui and 1caKacgf', fol lov;ed 

is "carcfull turned on incc thi~ i~ the t 

time that all the components (b hove workod tog.othcT in ;;i 

arvJ monitored for operation. Th<' instrum1.'11tatt0n vel'if1cat1on 

rurnent:ct10n point (1nc,luding sonic on the DRf>-1 

ion 

of SFM testing sets f'Dch 

and C0~1 slmnlators) to aJ1 allowable le,vels tu verJ fy that the 

wit11in fication. 'l'hc film-handling Gnis arf' for the f1 rst 

t cm level t.csts arc 

funct line the PPS/DP E.A.C 

tests, 'fhcto is no post-v 011 SE~l test, 1 fiOSt-vibration 

ls accornplishf'd at thi/ PPS/DP LAC lcv<"l where fo1:lu:r<" anoJys1s, 

4. 3.3 \ccoptD.;tce Testing 

tt'Sting 

ir and reTh? DRJ"1 consists of t1<0 satellite reentry icles (.SH.V 1 , an cj?ctahlf> 

er adapter (FA). After rccc t from the niantifacturcr, "'* 

ins t Jc 

4. 3. 3 1 LA anJ FA ;\cccptm'tc Testing. The EA/FA ar:d 1.J.fftncl seal and ri/cord 

assemb and test flcn~ is shown in gure !t.4-liJ. As a of 

th;;: receiving inspection proc:P<iur:·e, and also follov: J1D. inti ng strr1noe 

and insta1Jation of the 1"SBT assc-mhlic!), the FA and F1\ arc tested for: 

(1) LlcctTical co:;t 

( lsolatlon res tones 

(SJ 

( 4) 

Bri irt' ri/sistance of the 

11n 

'Rci'cl'eac·e -,··~........-=:c:-icc::-;--

echnic circuits 

**Genera l Electric Reentry and Environmental ems Division 111anufacturc'S 

SRV 1 s. Lockheed Ml:ssilcs aild Spar.::c Compnay mom<r1coturcs th,; E:\ and l!;\, 

4.4·21_.---

~-~1 _£__ 

Approved for Release: 2017/02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
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Bl 

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TO,._ !itCiler- c 

e1 "-OOS- w-c·-__ 91 

(4) Leak :rate of the film enclc.sure 

Hig:h-rrre.ssure 1 check of the n and 

(6 J Reentry prograrrrmer function 

Following an O'V£-'l'all 

SE}.1 and CO~l. 

in>pBctlon, the DRM i. s ready to he integrated v;·J th the 

4 .3 .4 Photographic 

(PPS/DP LAC) 

load SectiGniDual Platen Extended Allitudc Capab111 

'fhe PPS_/LJP E,\C is assen1bJeJ anz'. te::;ted in accordonce 1-:ith. the f1o;., plan sho\<n 

ir: figure 4.4-13. ,\brief description of each step ir1 the f1ov; yla11 ;is 

'>resented hy TnlJle 4.4-1, 

final assembly begins v.ith 111at1ng of t COJ\-1 to fonn the SFM/CO}.l unit . 

The broomsTic.k test which sirr:111ates hoT-clogging Js repeated to there 1s 

no hetween the COA and external structure (reference paragraph 4.3.1). 

An Ixx va1ue is dete~-mined for the SFJ\-1/COJ'.t usin~~ the test SP-tup shown in 

F "1.4-14, and combined Kith the lxx value of lhc DR~l (re<c,ence parBgTnph 

4 :; . 3,:;.) to 0hta in an over aJ 1 T xx vo 1 ue for 1 he PPS/LIP EA.C. f>,ft.cr SE~l/CD}l test 

i<1g, the Dlt\1 is rnated to thq SLf>l/COi-1 and the PP~/DP E.t.C for testing. 

Figure 4.4-15 scnts a vie';; of the <;\,Ssembly area •1.l1e:::e PPS/UP EAL 

Prior Lo PPS/OP EAC functional tc , test5; ar1~ performed 10 validate the SE'.'·l 

post-vibration condition and D!Th1 ,post-vibration film tracking. (TrBck 

tests a1•e dererred to t.hc PPS/DP EAC """"guration so lhat tf,cy uiay bt' performet'.. 

on a un5 fied 

Functional 'test 

1m-hancil 

of th.e PPS/DP LAC encompasses exercising a~- 1. ,'L'S/DP E,\C 

the SRV ocqcccrtcris wh'lch are checked :;cparately (i;.LCAL te:;,tin 

'1.4-26 

TOP SF'ft!T" 

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-

C05097360 

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CD CD Q) Q) 

CJ) CJ) 

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Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
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14 

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~T 5 I I 

'fest or Procedure 

5 TRJ\CKTNG SRV 1 2 

Art extens tr;;i test is :r1Jn at to 

camera and film han<ll 1;1g operation in the st1·ip mode. 11stments are mnde, if' necessary, at tilt frame couplers and RAf<i. The 

RM1 fired i ntc SP.1! 2 is in the !'>amc· 

for SRV l t rac1k111g 

ASSEMBLY Fl 

9 and 5 Jm re1nm'ed from both tak1a-11ps, The 1m from SRV 1 

is 

is 

and the 

iced to SR\' 1. 

test film evaluated. The 

16 A.SSFi\ffiLY RFFORBISHFS 

17 FlLM TRACKl?\G AFTER RESPllCb 

Short trucKJ.ng test ftrr 9 and 

1er11r nrnn1•r opa11at'.ion 0 rtBr 

5 fi1m·11andling :system5 is 1'Uf1 to 

lm ce ond refurbishinerit 

18 COMMAND MONTTOR CALIBRATION' 

20 

21 

.i\11 levels of command 

and 

.l\sseml) installs a 

n\onitors • s) possible arc comma11de<l 

al data track asse:mo1y at the to ul lo\\ 

data to be placed on 9 5 at the R!\M locatlon 

9 'ft<-tckln,g test. 

9 5 B.'SELJNE 'I'RACKING IN Arn 

run Jn the s mode with 

ON, This test is run in the +Y and 

the camera and RAM tracks 

+Z orie11tation Fvali..<ati0n of 

9 and 5 f111'.i1 is made attor.film re•tm1al 

ments are 

ur;I'f CONFIGtJRLD FOR RAM FlRE IN VACUUM 

is ir,stall 

4, 

Approved for Release: 2017/02/14 

~ C05097360 

to ireH<1rolr ,,;.1 BYEMAN 

(;ortro! s.~t'}"' (;; 

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T~_c_· 

TABLE 4.4·1 (CONT'D) 

T'est or Proced11re 

and all FSE covers Bre toruuec dov..11 with fSE vent 

i11 the is lowered to less than l mm 

stereo servos, 9 

5 SRC is perfonned, 

moto:cs is also 

5 slit muchanclsn1s 

C111·rer1t test foY crab 

23A HEATER TEST 

24 & 25 

and ground heBters are or•e1·oted and currents mc•cs"red 

each branch and zone. 

for 

INTERFACE 

This to::>t :is ne:rform·2d 

comm:tnds fTnm~ both 

test is then 

at h \n::; and low cu1"r0nt f01 ;111 

.-xcc;1r the r0chnJ c f:;nct:i ::ins, The 

at low vol and curre11t, 

F 

26 SOLAR ARRAY 'POWLR TCS1'INC 

27 

28 

f<la power to the PPS/DP LAC is varied a del tP of or 

3 volts every 0.1 - 0.2 second around normaJ vol wl:il'e 1 PPS/UP 

EAC s terns are CX•PT(1l 

9 5 5 

1'.his test is similar to air ba;i>2l in,~ test. Test i.s p<10'.1·0o:n;;td 

unit in +Z o:rientat 

wj 

Filn 

$ 

f\'V'JVlS 

r 

i;> .CUtl <tt 5~'!$Y.11 

1.-:11'' altit1.idc noxr::i:: 

c error data. 

Each in the high al ti tu.do :1orrru11 

j::; TtJJ1 th:rcc tilllCS at VtlYj 

4,4-33 

Approved for Release: 2017/02/14 C05097360 

!i<1nd1t 11111 BYEMAN 

Cor1trol Sy'>t;;m O~!, 
Approved for Release: 2017 /02/14 C05097360 

l 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

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ET 

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Approved for Release: 2017/02/~~ ~05~£ 

Tr•,RET 

BIF-OOR- K-C-019842-Rl-80 

4.4-1 (CONT' 

Block 'fest or P:roced1rrc 

vol tog cs. 9 and 5 lm trackjng is run for strip and short burst 

t lmcs. Thv 9 ar1d 5 l t bl a des are cl . 1~hc y; tcr0.o mi Tro:r hoot 

assemb is insta11ed and crRb servo rirn to 

51 ASSEMBLY LOWERS UNIT 

Remaining par1cls arc i11stalled anl tht:: 

Titc unit ls 1novcd tunnel for 

ectab1c 11at;;h is :installio:d, 

tcstJng. 

52 FUNCTIONAL 

53 

54 

56 

All systerns are exurclscd 

:rur, fr-c.:n extreme t•J i'.xt-remc 

SRV's. 

sides 

eTuted. TI1is test is perfow.ccl, at ambient 

servo systems are 

of cn.c:1 optcmi;,01·~1:u1:c <t>1<l pressure. 

seq11ences which are pecu ar to cld operations are r1111 at th 

s includes the Functional Tcsl (slniilar to Ft111ctiona 

lnt<;r1eoct it:::!, tes :s 

1'he Inlcrr{;actlon tests 

verify that the PPS/DP 

J-Je:: l th 

:run sc-v<.::tal 

Eil,.C an<l Control 

various arc or,ei·at.h1e 

from the factory 'fest boca<1sc vf u11it 

:simulta:n~ous to 

Section function norinalJ y when 

I11c Fu11c~i011al Test differs 

ln Field which 

can :tcsul t in and lin s appag 

F llm ln 9 and 5 ilrn-clrivc ems is to 1 t fx-om u 

bulb on the primary 

111t1;c ·Jl'al-1nted f,.:ir 

mirror a specified period. This -fi 1m 

iYH.licati.uns of silt bl:.i.tlc co11tatn.1.natio,1, 

ASSEMBLY REMOVES PILM 

Film is rernovi:Ji ;_;RV l u11d sent i'or pro.;.'.ossi11g. 'f110 -f1lm is 

resy>Iiced to SRV 1. '!'he p1·0<1e1;s1"! fi]m is to eva111ate 

FTL~J TRACKING AFTER RESPLICE 

Sho1•t track 

vci·ify 

test for 9 and 

OP•Cn•tfon :tt rospJ. 

4. 4- 37 

Approved for Release: 2017/02/14 C05097360 

crn is :r.un to 

an<l S/C i·cfu1·b:.t$llll1cnt. 
Block 

57 

58 

59 

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~ETC 

B I r . 00 8. ..;_Vi_· c-=-·_;O_l .:_..;__,_· -" ·_, ·-"-'' 

TABLE .4.4-l 

BUY OFF 

Unit off by the Air Force. 

EI.ECTRlCAL CONDTTlONINC 

11\e unit is electn•cocLLy; and then brid1ge14i1•e, drive 

line rcsista11ce) no voltage~ ilnd solation measurements matle with 

DTU off po1 .. 1er np11li 

DECABLI. UN!T REMOVE PROM 

Unit is xcturned to stor11ge 

60 STOR/\GE 

()2 

a 64 

65 

Ur• 1 s in the c ---roo1n or tent on an erector truck. 

Every 7 the 90 de9r1res. The unit is stored 

on an erectox truck quick reaction to perform vo:rti-cal 

i:f the unit i:: called up usoge, 

Assemb removos unit from sto:roge tho 90 ex;orco1so. TI;e ma 

hatch is removed and the unit erected. 

VERT! 

Vi ewrm:rt door nerf<}1'.1lled to sotJ !\Tl' and 90-<lay 

requirements, This ing at high, low, nominP 

and at least 90 Prinlarv and motor ON time. 

strain and finalizes COM Arca. 

ASSLMBLY LOllLRS UNIT 

storage 

'.to 1 tage, 

y 

Rema panels arc iet:U1ble tch is installed, 

unit !llOV!i:d l 

CAB PREP FOR VACUUM 

Unit cBb 1 ed: cables connected to SRV l 

4.,4~ 38 

~~ Approved for Release: 2017/02/14 C05097360 

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73 

74 

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8 i f.-ODS· ·----l_11_9_B_4_1_' -_R_I_-_s_c 

1·ABLE 4.'1-J (CONT'D) 

o:r Procedure 

SLIT BLADE CONTAMINATJON TEST 

FilJJ1 in the 9 411d S 

bulb on the primary 

l«tt~r eval<JU1:eo 

· Unit :rctu 

testing; 

to amb 

a speci 

cac"lms '{)f sl 

is cd to i10ht from a 

perio,J. <Di film 

blade co11ton1iru1tiot1, 

75 ENVIROJ\1RiE!\TAL LAB ESTi\BT~ISHF.S VACUllll-1 IN TllNNE·1:/·' 

7'7 

78 

to less. than 1 ,mm hg. 

SRV 1 SRV 7 TRACKTNG 

9 fi lm-handl in the mode lnto SRV l to 

· ·verify proper s, ther, and the. tracking 

·test repeated iritc SRV 2. sequence is repeated for the 5 film~ 

haridl sys teni. 

ENV!R01'~1ENTAL LAB RE111RNS-THNliEL TO ATMOSPHERIC. l 'RESSlJRE, 11JRNS OFF 

. ' " ' 

Tunne'l pressure is rctur:ri?d' to. aTnbi .:::nt cor1d.i ticms ·coo 1 

tur1nel is · for testing. 

Jn 

RCMOVC Fl RErURBJS!l RAM RESPL!CC 

.. '· t'<iln1 renioved from SRV 1 a·n«J ?. • 

for l"ITOCeS!>l j ng. The f J lm j 5:. r:espl j ceJ 

RAM. The pr<:ice;:;:.sed ,.,.,,,~,,s check 

contam:lnation 'test., 

. , ... ,, Tho lm f:rof!! SR:V 2. is sent 

to S.kV 1, Assembly J 

to evaltt.ate rP of 

tluta the 90-day cycle is reviewed, 

FIU-1 'l 

Short t test for 9 and S 

prope1· operation afte1· film re 

film-handll11g systems ru11 to verify 

ice and S/C refurbishment, 

Har.ale: "';i BY£MAN 

r.o .... !rcl s,sh::" C> ·1, 

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82 

83 & 84 

86 

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~(; 

'l'ABLL i;.4-l (CONT'D) 

'fest or 1-'rcc:edure 

;\~:;cu;11 l:y :ce-mwves unit: f'rorri 

he,tch is rer:;oved and the unit 

fo::r final vent test. The main 

VF.RTtCAL '1/Tl::WPDRT DOOR 'I'EST 

testJng is perfoTmed at high, Jow, and nominal 

fo1111s strt:in gage nteasurtJiif'nts and finalize;,; C01'1 

voltages. 

,.\rea. 

lJNT'l' 

Remuining panels are installed and the ejectable hatch is installed. 

1'11B u; if, 1n.:-1ved into the tunneJ for fi11al testi11g. 

UNIT PREP FOR 

!J;ij t J,$ 

SH\" 2 

cable·i 'for t:JstiDg, FlJTF cables connected tn SRV l an<l 

«6Ccpt.acJi's. All FSF covers torq11ed down with +Y FSE vent 

ENVlfz(Ji'Jj\JL:\IAL LAB L(JWLRS TUNNEL 

11J.e Df thn test tL'H!l(;:'l ls set to 

t0 allor: checkout i:ronmento:l 

0tht1~' ·~est ,tt this low te:npornture, 

- (>lP, TI1is is 

tem nnd to 11erfnTm 

87 SRV l ft 2 SHt)RT CYCLE 

89 

FunctJ,;:y,1111 ng of the nornaf (primary rnode) recovery sequence 

Sf\\' i and SltV .2 is perfoxwcrt • 

'fhe in the tunnel .is .lc>wc:rc'd to less 1 lf'Jn hg:. 

288 1 C/D 

This test is 

l/f C01'.llll8:<ldS 

i1erformed 

fron: 'both 

at nomina1 voJtage~ 

decodBrs .;-;x the 

Approved for Release: 2017/02/14 C05097360 

snd lcw current for all 

pyro ions, 

K<r-1:ii t .-1 a BY EMAN 

control Systtw 01'\I / 
Approved for Release: 2017 /02/14 C05097360 

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I 

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~-Ji_ 

TABL!: 4.4-l (CONT'D) 

Block 

97 FIL~i TRJ\CKJNC; i\PTER Rf;SPLICE 

-rr1n to verify 

film 

9B fiA'lA REV lE\•}1.J!) 

ion data is reviewed with Air Frrt'CC, 

excess 9 and 5 filni, ahcvc th~ operationol tise figure, is :run 

intc r;r.v ~, B:.rst r-inJ r.t;·in modes of erat Ion art' u:; t0 '.run 

I, 5$ 10, 20, 50, or 100 foot lengths as 

100 ASSEMB11 REMt.Y\iliS FIL~1 FROM SRV 1 

9 and ;; fi. Jn1 5 s 

101 

102 

103 CO:\f<JTI 

DTU of'f 

104 TJNI'f 

\Jn5.t i:> tunnel the 

105 FI Li>[ LEAK RATE 

1'he test 

4.4-43 

Approved for Release: 2017/02/14 C05097360 

~\nd tltcn 

s.yst<:lhs run 'to ve:ri 

brJc<l•ew:i1·e, d 

;,'i t'.!1 

l ! 

pu;nping 

line 

to 

!'14~(llf Y•<l BYE.MAN 

ec~tr01 ;Jy~.t<:!l': Ori y 
Approved for Release: 2017/02/14 C05097360 

T~T 

TAB LL cl .4- l (CONT' DJ • 

Block 'rest or Procedure 

1:1 

2 inches 

seconds. 

of water 

'This 

pressure 

dnne fnr 

and 

+Y FSF. vent 

pressure 

capped and 

drop 

11ncapped. • 

106 & 107 ASSE!vlBLY SHIPPING PREPS 

Final assembly preparations c,f t<nit prior to shipment. Checkout of • 

trailer and ship11ing conta~.rter performed. 1'he FPS/DP EAC i:s place~ 

into the containc:r and the container loi1ded onto trailer. 

108 SlflP!'<1EN1' 

Approved for Release: 2017/02/14 

~ C05097360 

liar\clr v1~ BYEMAN 

V;;nt,0! 3·1•,tqn: C"i' 

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• 

• 

• 
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Approved for Release: 2017 /02/14 C05097360 
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T 

Approved for Release: 2017 /02/14 C05097360 
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T 

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E 

Approved for Release: 2017 /02/14 
Approved for Release: 

Bl f ' "" -m~W ______ .,. __ , 

Block 

7 

8 

ll 

12 

13 

14 

•;J; ',, :'{ 

TABLE 4.4·2 (CONT'D) 

9 AND 5 ING IN AYR 

PRcP FOR VACUUM TEST 

All f'SE covers 

111 the tunne 1 j s lowered "n,'"1:J )', :;,: f:,ii 1-_\) \'\;'•,' J, 

S BASELINE '!N''VAJ:tfuij' '''"" ·'° • 

This test is 

with 

'",],,,,'' '(''""'"' 

similar to 

-~f 0:10cn1:,e,;:.t<m,,""> .,..: .. 

l'I CON'l'Af.tlNA'I'lON 'i'ES1' 

re1sp1iced to SRV 1. 

Approved for Release: 2017/02/14 C05097360 

,, ,I 

G -

W-C-019842-RJperformed 

is 

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Contro\ Sy~trm Ori f 

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Approved for Release: 2017/02/14 C05097360 

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TABLC 4.4-2 (CONT 1D) 

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!1BCABLE UNIT, REMO\'E PR\'111 TUNNEL 

Unit: ·s.YE'illm1ed oo:r t~~~t /' 

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CHANGE TRUCKS~ EP1'.CT lJNIT 

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:requ,i :red vertical assemb 1 v /test. ?l'.e11·n11.i_13n:s._ 

LOWER UNIT INSTALL PANEL AND 

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Approved for Release: 2017/02/14 C05097360 

t \ ; ( ;! 

lied by' As1senmly, 

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Hiind!t via BYEMAN 

CoritrtJ\ s,,nl<'m 011\y 

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Approved for Release: 2017 /02/14 C05097360 

Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017 /02/14 C05097360 

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Approved for Release: 2017 /02/14 C05097360 
Approved for Release: 2017/02/14 C05097360 

h. Exercise of all motors> 

cm1 be act conslst,<:;I~t )w,~th 

'rhe l/iewr•ort 

c hid<"! becBUse 

BIF-008-

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te;;t 

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in vacuum. 

tested. 

PPS/DP EA.C Acceptance 

is also verified. 

Proper operation of electrical systems 

The conflgu:rat thls test d ent 011 whether tbc unit being tested 

is a primary unit or backup unit. A urimaTv unit is the next un1t 

to be sliipped. 

at clean Toom 

on unit is done at 60F. A backup unit is tested 

and sure, 

The 90-day 

a quick 

ex ere 

Due to u 

9 5 

the same 

hll. 

on the PPS/OP E.4.C Test Jiluw, 

turnaround in case a unit is cal led up for 

or 21 <lays 

e of 9 and 5 prime film 

film may be 

test flow has been planned 

an th at was used to 

test. 

the 90-

call up 

and is detailed 

ly load 9 

4.4-54 

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Approved for Release: 2017/02/14 C05097360 

4.4-13. This enables 

usage a 90-day 

in 

s 

rel0ading 

unit. 

n1iure 4. 4-14. This 

pr loads. 

Kand!e via BYEMAM 

Cl;lntrol Syslern Only 

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Approved for Release: 2017 /02/14 C05097360 

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Approved for Release: 2017 /02/14 C05097360 
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