APS PROPELLANT
TABLE 3.2-17
MISSION J-2
LM-II LOAD CALCULATION
i. Full tank - Item K, Table 3.2-16 (ib)
12. Density of off-load tables at loading
temperature and pressure (ib/ft 3)
I 3. Propellant volume (divide item i by
item 2) (ft 3)
i 4. Measured density (from Table 3.2-19)
(lblft3)
5. Resulting full tank load (ib)
* 6. Off-load amount (ib)
7. Propellant required to fill RCS manifolds
(ib)
8. Propellant load (ib)
DPS PROPELLANT
9. Full tank - Item K1 Table 3.2-16
Ii0. Density of off-load tables at loading
temperature and pressure (ib/ft 3)
iii. Propellant volume (divide Item 9 by Item
i0) (ft 3)
112. Measured density (from Table 3.2-19)
(iblft 3)
13. Resulting full tank load (ib)
14. Off-load amount (ib)
15. Propellant load (Ib)
RCS PROPELLANT
P. V. Calculations
Amendment 114
9115/71
FUEL OXIDIZER
A. GSE Volume (in3 )
B. Initial Ullage Pressure
(PSIC)
C. Initial GSE Pressure
(PSIC)
D. Final GSE - S/C Pressure
(PSIG)
E. Ullage Volume (in 3) - Solve
the following equation by
substituting the values in
the indicated steps.
Ullage Volume = (D-C) (A)
B-D
NOTE :
Fuel Oxidizer
Tank A Tank B Tank A Tank B
IThese items will be completed only if a density sample is not
made prior to loading. If a density sample is made prior to
loading, then the items will be left blank.
3.2-108
SNA-8-D-027 (III) REV 3
