user manual

_nendment 74

1/14/70

MISSION H-2 MASS PROPERTY DATA TABLES

Unless otherwise stated, the controlling vehicle propellants are in the low

end of their tanks and the passive vehlcle propellants are in the high

end of their tanks.

Table 3.3-20 presents CSM-109/LM-7 (docked) mass properties, in Apollo

coordinates, as a function of spacecraft weight for the

Hybrid SM/SPS burn.

Table 3.3-21 presents the CSM-109/LM-7 (docked) mass properties, in Apollo

coordinates, as a function of spacecraft weight for L.O.I.

SM/SPS burn.

Table 3.3-22 presents the CSM-109/LM-7 (docked) mass properties, in Apollo

coordinates as a function of spacecraft weight for the

D.O.I. SM/SPS burn.

Table 3.3-23 presents the CSM-I09 mass properties, in Apollo coordinates,

as a function of CSM weight for the Circularlzatlon I SM/SPS

burn.

Table 3.3-24 presents the CSM-I09 mass properties, in Apollo coordinates,

as a function of CSM weight for the Plane Change I SM/SPS

burn.

Table 3.3-25 presents the CSM-I09 mass properties, in Apollo coordinates,

as a function of CSM weight for the Plane Change II SM/SPS

burn.

Table 3.3-26 presents the CSM-I09 mass properties, in Apollo coordinates,

as a function of CSM weight for the T.E.I. SM/SPS burn.

Table 3.3-27 presents the LM-7 mass properties, in LM coordinates, as a

function of LMwelght for the P.D.I. DPS burn.

Table 3.3-28 presents the LM-7 ascent stage mass properties, in LM coordinates

as a function of weight for the lunar llftoff APS burn.

Table 3.3-29 presents the LM-7 mass properties, in LM coordinates, as a

function of LM weight for the C.S.I. to docking LM/RCS burn.

3.3-64

SNA-8-D-027(III)REV 2