user manual

Amendment 08
1/22/71
SUPPLEHENTARY DATA APPLICABLE TO SEQUENTIAL MASK PROPERTIES TABLES
General Comments to be applied to Tables 3.4-1 through 3.4-8:
Inertia data dispersions are +10%.
m
Dispersions shall be used as 3c deviation v_Jues.
All initial propellant weights are total tonked.
The (+) or (-) si_ followln8 the name of an item indicates that
the item is added to or subtracted from the preceding total.
Table 3.4-1
SM/SPS simbal angles for SPS abort sequence _re: Pitch - -1.417 deg.
Yaw - 1.315 des.
Table8 3.4-7 and 3.4-8
CSM and LM consumables changes are pre_ented in Tables 3.4-7 and
3.4-8, respectively.
Tables 3.4-4 and 3.4-5
Delta Z
LES motor tilted angles
(Delta includes 0.3 deE. for
down range dispersions)
LES motor tilted confluence point
PO_ motor tilted 8nsJ.ee
PCM motor tilted confluence point
- 0.85 in.
Delta = 2.260 des.
Sigma - 273.810 des.
X -1222.300 in.
Y = 0.043 in.
Z = 0.280 in.
Delta = 89.i60 des.
Sigcua = 270.000 des.
X =1429.000 in.
Y - 0.517 in.
Z - 3.320 in.
The docking probe and rlng are Jettisoned at t-14.0 seconds in Table 3.4-4
and Table 3.4-5.
I
3.4-1
SNA-S-D-027(III)REV 2