Amendment 98
1/22/71
TABLE 3.4-14
Command Module RCS Loading Parameters and Calculations
This table will be completed when loading is accomplished. For Mission
Planning, reference should be made to Section 4.2 for nominal load, loading
tolerances, trapped and deliverable propellants.
FUEL OXIDIZER
Tank k Tank B Tank A Tank B
A. Tank Volume @ 0.0 PSIA (in 3) 1472.8 l_ 1/_ /._
B. Liquid Line Volume (in 3) 21.0 17.4 17.1 16.4
C. Total A + B (in 3) 1493.8 1491.9 1806.0 1803.9
D. Initial Weight in Bleed Unit
Prior to Loading (Ib) 150.0 104.7 _
E. Final Weight in Bleed Unit
After Loading (Ib) 105.8 60.5 119.8 39,7
F. Propellant Load (item D less
than E Weigh Tank) 44.2 _AK2- 7s_2 78.3
G. Propellant Load by P.V. ___ 44_5 78.6
H. Loading Temperature (=F)
70_0 7on ___ __X2.AI
I. Specification Propellant
Load @ 70e5"F (Ib)
_._.9 -._.9 _.__±1.6 7A _±1.6
J. Total CM/RCS Propellant
Load from Item G above (lb)
88.8 156.7
23.1
133.6
K. Maximum Trapped Propellant (Ib) 13.3
L. Nominal Deliverable (Ib) 75.5
3.4-90 SNA-8-D-O27(III)KEV 2
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