user manual

Amendment 74
1/14/7o
SUPPLEMENTARY DATA APPLICABLE TO SEQUENTIAL MASS PROPERTIES TABLES
General Comments to be Applied to Tables 3.3-1 through 3.3-8:
Inertia data dispersions are +10%.
Dispersions shall be used as 30 deviation values.
All initial propellant weights are total tanked.
LM propellants are assumed to be in the low ends of their tanks except
when in the CSM/LM docked configuration. In the CSM/LM docked con-
figuration, LM propellants are assumed to be in the hlgh ends of their
tanks. CSM propellants are always assumed to be in the low ends of
their tanks.
The (+) or (-) sign following the name of an item indicates that the
item is added to or subtracted from the preceding total.
Table 3'3-i
SM/SPS glmbal angles for SPS abort sequence are: Pitch = -1.530 deg.
Yaw = 1.315 deg.
Tables 3.3-7 and 3.3-8
CSM and 124 consumables changes are presented in Tables 3.3-7 and 3.3-8,
respectively.
Tables 3.3-4 and 3.3-5
Delta Z - 0.75 in.
LES motor tilted angles Delta = 2.124 deg.
Sigma = 270.121 deg.
LES motor tilted confluence point
X - 1222.379 in.
Y = 0.001 in.
Z - 0.224 in.
PCMmotor tilted angles Delta = 89.324 deg.
Sigma = 270.676 deg.
PCM motor tilted confluence point
X = 1428.970 in.
Y - 0.O18 in.
Z - 2. 662 in.
The docking probe and ring are Jettisoned at t=14.0 seconds in Table
3.3-4 and Table 3.3-5. Reference Memorandum EX24/8912-344B, dated
December 4, 1969.
Table 3.3-5 includes a rapid depletion of CM/RCS oxidizer from t-0.0
to t=9.0 seconds and of CM/RCS fuel from t-5.0 to t=14.0 seconds.
3.3-1 SNA-8-D-027 (III)REV 2