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SA-1 Press Kit

Date post: 10-Apr-2018
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    . -.I , -. .

    - Verify s t r u c t u . r a l i r . t e g r i ' ~y of the vehicle s ~ L r T r a r f i e ,evelueting s t ress at c r f z l c a l xcfien'r;s of flight and Ceter-minr;nz vibration and Sending values

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    . .- . -.- . ,

    A t o t a l . of about 610 channels ~f L-nformation w i l l be tele-me' ie?ea f r o n the Sa tGm vehicle Urmediateely prior t o azd Curins thif l i g h t ./---, 1-3LJ

    1 . A

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    I

    $21 measurements.

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    I 9 , .I I ( .\

    . -c

    .-\,L/'

    ...T-570

    G

    i\"-2.26T-80

    "-60

    ,-

    T-210,

    T-130to T-75to 570

    y-65t o T-30

    T-50T -5 :14:.T-0 :25T-0

    Xemove l a s t service structure pla-cfoyrnRemove service stbuc'cureClear lzunch pzd areaSecure launch c~ntrol e n t e rCoqlete loading liquid oxygen (replenish to l i r ' t - o fPressurize various gneumatic systemsFis?ing caimiid! ar,d au tomat ic sequenceR e t r a c t long c s b l e boozIgnition

    Phi;. engFnes are lgnited io- p a i r s -- each -pair sbou'c a & -%aldLtho f 2 secor-d after the prev ious y i u . , AfJcer Pgn i t io n th e r~cke ' ; ; sha16 on ~ ' c s sunch ing pedestal u n t i l pu.oger corc?ms'i;ion is achieved' ,Lx ll enzines. The hold-domi pe-liod n o m a l l y will n o t exceed

    d" four seconds.

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    . .c . .

    The f i r s t t e n Sa turn P l i & t b o o s t e r s & r e bei2g prociuced at 3S??CL a t e r o m s will b e prochced. b y a concractor now in process of Selec-Liiat NASA: s large r o c k e t asse;:iQr p l a n t bt?fng estcblished at t h e HichoxCrdnence Plant, New Orleans, -2 ...

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    CONTROL

    S r t ~ i r n i l l G S ~l l - i n e r t i e i gsiC.ar;ce e r!lor+e ~ & m n c e d ardr/!areb e intTod-ccad ii?i;o t h e system as t h e gd iCance niss io izs becorn2 moredelmandilz~:. CSjec'c of the guiS?ar,ce schene i s 'm provide a uf i i ve r sa lsystem t k a k is capable of per fom i f ig a vzrd.ty of mLssLon requirementsp i a c e d on t h e v e h i c l e 'GO meet p a y l c ; ~ d b j e c t i v e s , This universzd.rruidance concept w i l l allow a v a r i e t y of pequixwxents w i t h ii. miiziwmO.cnanzes 0 O r

    Iieert of the 2 i n a i guidance scheme is a high-speed dlgital c o n p uinco-por+atins advanced techniques of & s i p ar-d packzging and capable 0ncecing Sa ' cux s high r e l i a b i l i t y s t ~ n c k r d s nd d i f f i c t l l t nlss ions in

    2-4.

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    ON

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    t0 :.;,:;,. ..,

    , ., :, t!....... . .

    ?2-0

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    i

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    X.L-S-4 has announced p l z n s ?ai' t h e a c q L i s i t i o n o f s m e 80,000a c r e s 2o-r this expansion which cove rs lands n o r t h and wzst ofp r e s e n t C;pe f a c i l i t i e s .The p l a m e d complexes w S l l be a base fo-r maaned l u n s r;'lights and o t h e r miss ions requiring zdvanced SctuFn and Xova-c l a s s boos-Lex.

    Service Struc 'c~ l re - Tke s e w i c e structu~q s 310 f e e t tall,T'c has 'w in l egs measuring 70 feet by 37 f e e t a-l t h e base,cen-Ler opening;, i n which t h e rocket i s s i t u a t e d d u ri ng checkout,i s 56 f e e t wide.

    The

    3-2

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    k.__.

    -_',,

    .-.~ ~ e d e s t ~ l- The pedestel is l o c a t ~ d n the center or" tne---l a i i n ch ped.>=,c-destzl oundatiiol? contzins 43400 cuSic y a r e 3 o f c onc re te 2nd$30 tons of' s t e e l .center t o f'0U.i. Tee'; zt the edges.

    Bolted to a E L ~ I ~ t t h e t o p of t h e p e d e s t a l are e i g h t a:ei?~s,F ~ u r ~ ~ 3q q o r t a r m m d the c'cher r o w Sozh suppoz+tthe rocket2nd r e s t r a i n it fron 1ir"toTi' uxtil t h e p ro pe r b u m k g condi tFonh a s beer. achieved by a l l e i g h t Saturn engines.

    3-3

    it is 4.2 feet ~ q u a egd 27 Zee t high. TheI t s d ep t h v a r i e s fY . o iX eight f e e t zt th e

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    Ikc inm in~--. Basin - - PI s k i x n i q basin Ls located about 300feet Prcrn zhe edge o f thz pad on ;he beach sLde. Tkis v z t isusea to collect ?-del which-might be spilled on th e p d , t h u sprevent if iz it f rom enter ing i - j ~ ~ ; - i z a lape ci+aina?e car,als.

    d -Q

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    * . . . - , . , . *

    3-5

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    '. ..

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    ,-il;

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