Apollo Saturn User Manual Page 39

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SPACE VEIIICLE WEIGHT VS FI.IGIIr TI:.I}"
l.l,iir, stage pr'pella1_ c_,' u;_4_ti,,.: du_i1_ F, S--]C pc':ercd fl_[.hr (approxi-
mately 161 second.;) is apprc.xlmnt¢.ly :,,67.'J,300 pounds. Propellant consumption
during S-I I po;'er_.d f_i}9_t (;,ppr_,._t;_m,:Iv 3_9 seconds) is appz'oximately
971,_50 pounds. Duriqg S-IVB powur,.J fl;::ht, lncludtng first and second burns,
(approximately 46] sccond:_) the propellant co,_sumption is ,.pproximately 223_900
pounds.
Vehi__cje We___/llhtData_(,A;_d)roxlrn:,te) Pounds
Yoial ut S-IC ISnILIu_, 6,484,300 .
Total at liftoff 6,398,500
Total at S-IC OECO 1_826,900
Total at S-If ignition I,h53,800
Total at S-II OF.CO _69,700
Total at S-IVB Ist ignition 367,C00
Total at S-IVB Ist ECO 297,500
Total at S-IVB engine restar'. 294,600
I
i Total at S-IVB 2nd ECO 133,600
Total at S-.IVB/CSM separation 130,900
Total at SC translunar injection 100,800
1970011707-039
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