user manual

Amendment 79
3/30/70
TABLE 3.3-15
SERVICE MODULE RCS LOADING SU_4ATION
This table will be completed when loading is accomplished. For Mission Plan-
nlns, reference should be made to Section 4.2, for nominal load, loading
tolerances, and nominal deliverable propellants.
quad A (ib) quad B (Ib)
Secondary fue_ 40,2 Secondary fuel* 39.8
Primary fuel 70.2 Primary Fuel 69.7
Total fuel 110.4 ±0.7 Total fuel 109.5 t0.7
Maximum Trapped 2.1 Maximum Trapped 2.1
Nominal Deliverable 1083 Nominal Deliverable i07t4
Total Oxidizer
Maximum Trapped
Nominal Deliverable
225.6 +2.3
A.5
Total Oxidizer 22_,5
Maximum Trapped 4.5
Nominal Deliverable 221,0
*2.3
Quad C (Ib)
Secondary fuel* 40.0
Primary fuel 7U.l
Total fuel 1101'0.7
Maximum Trapped 2.1
Nominal Deliverable 1080
Total Oxidizer 225.4 '2.3
Maximum Trapped , 4.5
Nominal Deliverable 220.9
quad D (lb_
Secondary fuel*= 3g.8
Primary fuel I0._
Total fuel Ii0,i
Maximum Trapped 2.1
Nominal Deliverable i08.0
226.2Total Oxidizer
Maximum Trapped 4.5
Nominal Deliverable 221.7
t0.7
*2.3
Total fuel
Maximum Trapped
Nominal Deliverable
Total SM/RCS Propellant Load (lb_
440,1 ±1.4 Total Oxidizer 902.7
R_4 Maximum Trapped IR__
431.7 Nominal Deliverable 884.7
14.6
*Secondary fuel load for all quads determined by P. V. calculations.
3.3-56
SNA-8-D-027(III)REV 2
II