user manual

TABLE 3.5-10
CONSUMABLES LOADING REQUIREMENTS AND TOLERANCES
Amendment 86
9110170
MISSION J-i
SPS PROPELLANT
Pressure (PSIA) Temperature (°F)
Fuel Oxidizer Fuel Oxidizer
70+5 70.+_5
110±4 110±4
quantity
Fuel
See Figure
4.1-3
Readout (%)
Oxidizer
See Figure
4 .;-4
SPS Propellant Load (ib)
ILoad
2Trapped Outside Tanks
Tanked
2Trapped Inside Tanks
3Nominal Deliverable
Loading Requirement
Fuel
15704.0
78.6
15625.4
67.6
15557.8
Oxidizer
25092.0
123.7
24968.3
171.5
24796.8
Fue i
Actual
Oxidizer
_Service 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
Con sumab le
Helium- SPS Bottles
Helium- Fuel Tanks
Helium- N20 _ Tanks
_elium- SM/RCS
Quads A
Quads B
Quads C
Quads D
Helium- CM/RCS
Sys ten A
Sys ten B
Nitrogen - SM
Primary
Secondary
Loadin_
Pressure Temp
(PSIA) (°F)
3600 70
178 70
178 70
4150 70
4150 70
4150 70
4150 70
4150 70
4150 70
2500 85
25O0 85
Re qui remen t
Weiaht
(Ib)
87.6
5.4
6.0
1.3
3.5-71
Actual
Earth Launch Pressure TeNp
(OF)
Weisht (ib)
87.6
6.0
1.0
1.3
(PSIA)
SNA-8-D-027 (III) REV 2