user manual

TAllLI 3.5-17
LOAD CAL_TXOM
1. Full tank - Item K, Table 3.5-16 (lb)
12. Denslty of off-load tables at loadlnl
temperature end preosuta (1hilt 3)
13. Propellant volume (dlvtde Item I by
Item 2. (f_3)
14. Measured denslty (from Table 3.5-19
(lb/fc 3)
5. Rasulttns full tank load (lb)
6. Off-load amount (lb)
7. Propellant requlred to f111 RCS au.nifolds
(lb)
8. Propellant lomd (lb)
pPS PROPELLANT
9. Full tank - Item K1 Table 3.5-16 (lb)
I10. Density of off-load tables st loadtn8
temperature and pressure (lb/ft l)
Ill. Propellant voluDe (divide Item 9 by Ices
10 )(ft 3)
112. Measured density (from Table 3.5-19)
(lb/ft 3)
13. Resulting full tank load (Ib)
14. Off-load amount (lb)
15. Propellant load (Ib)
RcsPROFZLI_ST
P. V. Calculations
A. GSE Volume (In 3)
B. InitLel U1leSe Pressure
(PSIG)
C. Initial GSE Pressure
(PSIC)
D. Flnsl GSE - S/C Pressure
(PSZ¢)
E, Ullale Volume (in 3) - Solve
the follovin8 equation by
lubstttutin8 the valual in
the indicated steps.
Ullale Voluam - (D-C) (A)
I-O
NOTE:
Amendment 86
9110170
Fuel _ldlser .
Yuel Oxidizer
•_3.qnk_ tsu!_! _tsnk__ It_.._
1These _tewm will be completed only if a deem£ty smqple te emt
made prior to loadlnj. If 8 de_ity sample is m_le prior to
loadln8, then the items w111 be left blm.
3.5-82 SNA-S-D-O27 (IZl)UV 2