user manual

TABLE 3.2-10
CONSUMABLES LOADING REQUIREMENTS AND TOLERANCES
MISSION J-2
SPS PROPELLANT
Amendment 114
9/15/71
Pressure (PS IA)
Fuel Oxidizer
Temperature (°F)
Fuel Oxidizer
110±4 110±4 70±5 70±5
quantity Readout (%)
Fuel Oxidize r
See Figure See Figure
4.1-3 4.1-4
SPS Propellant Load (ib)
TLoad
2Trapped Outside Tanks
Tanked
2Trapped Inside Tanks
3Nominal Deliverable
Loading Requirement
Fuel Oxidizer
15704.0 25092.0
78.6 123.7
15625.4 24968.3
67.6 171.5
15557.8 24796.8
Fuel
Actual
Oxidizer
4Servlce Module RCS Propellant
Secondary Fuel - Quads A, B, C, D - See Loading Window - Figure 4.3-1.
Primary Fuel - Quads A, B, C, D - See Loading Window - Figure 4.3-2.
Primary and Secondary Oxidizer - Quads A, B, C, D - See Loading Window -
Figure 4.3-3.
5Command Module RCS Propellant
Fuel - System A and B - See Loading Window - Figure 4.3-4.
Oxidizer - System A and B - See Loading Window - Figure 4.3-5.
9Helium and Nitrogen
Consumable
Helium - SPS Bottles
Helium - Fuel Tanks
Helium - N20 _ Tanks
Loadin 8
Pressure Temp
(°F)
70
70
70
Requirement
Weight
(ib)
Earth Launch
Weight (ib)
Helium- SM/RCS
Quads A
Quads B
Quads C
Quads D
Helium- CM/RCS
System A
Sys tern B
Nitrogen - SM
Primary
Secondary
(PSIA)
3600
178
178
4150
4150
4150
4150
70
70
70
70
70
70
85
85
87.6
5.4
6.0
1.0
87.6
6.0
1.0
4150
4_0
2500
2500
1.3
Actual
1.3
Pressure Temp
(PSIA) (°F)
3.2-96
SNA-8-D-027 (III) REV 3
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