user manual

TABLE 3.2-14

MISSION J-2

Amendment 114

9/ls/71

CO_4AND 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 A Tank B Tank A Tank B

A. Tank Volume @0.0 PSIA -(in3)

B. Liquid Line Volume (in 3)

C. Total A + B (in 3)

D. Initial Weight in Bleed Unit

Prior to Loading (lh)

E. Final Weight in Bleed Unit

After Loading (ib)

F. Propellant Load (item D less

than E Weigh Tank)

G. Propellant Load by .P.V.

H. Loading Temperature (°F)

I. Specification Propellant

Load @ 70±5*F (ib)

J. Total CM/RCS Propellant

Load from Item G above (Ib)

K. Maximum Trapped Propellant (ib)

L. Nominal Deliverable (ib)

3.2-102

SNA-8-D-027 (IIl) REV 3

II E E L: E L L