Apollo Saturn Bedienungsanleitung Seite 45

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Seitenansicht 44
S-!rC ST.\GE PROPELLAI(T SYS'J t,7,I
Tile S-IC stage propell:,nt svstem is co:,lpnsed of one LOX tank, one RP--1 tank,
prope11;mt ]ines, control valves, vcnts, and pressuri_'ation subsystems. Load-
ing ol L0X and RP-I tanks is controlled by ground computers. RP-I loading is
completed approxii,_,r,tcly nine d-ws prior t_ ]iftoff. },OK bubb!in?, is startcd i
a
at the (,e,_:inningof LOX chllldo,<n operation aad is continued throughout LOX ._
loading and again before liftoff to prevent possible gcyscring. Prior to Jilt-
off the RP-I tank and the LOX tank is pres.qurized by hcl_um from a good source.
At liftoff the RP-] tank is pressurized with helium stored in bottles located in *_
o
the LOX tank and heated by passing the helium through.the heat exchanger. LOX
tank pressurization is maintained by LOX'bled from the engine and converted to
GOX in the heat exchanger. :1
S-IC PROPELLANT I,OAD A)_ OPERATIO'CAL SEQUEXCE _"
- --4- lj I ,
fOO-- " -- -- "l ...........
----j_,2o;_b,/,_;,_ 7 i- -
S+ar* A,A'om_+ I k i'¢"1"o_¢
'_'_',, I
so-- I I I
: ,o_ i ''1'
h3ni_';on Co,',,,_a,M
t // 94._,ooib-Y_in A I
0 I I
: I I :
zo-- I I
: I 6.5"/0
o I = ,, _.L-----14_zooI_/,_i_, I I
,,, _ i ......., I,,, ,I I
-9dli. -S.Shr. -4.q -I.0 -.4hr. -IOnia. -18,1_:. -72 -it "_.lt -/=,_ 0 |
' ' . ' I _ ' , I I
I i
I
Aa/,,_-l- ”$px7,,I i , ,
RP-I Loa,=l;^9
C.o_pI e..I-=d. I-il P,_s,,o,..;_,.
I : Tanv_ I_
LO_ Repienlsh
_- . _,--2 '_ - '
|LoX Buloblin_
L O_ -_6=r4 L ¢'a,_;a9
\ Sy_,_¢r,,_ LOX Pr_';,su,"i Tan k
" I GoX Pr_=suri'=_
TaaR I
44-
1970011707-045
Seitenansicht 44
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