user manual

Amendment 98
1/22/71
TABLE 3.4-8
LM-8 Consumables Change Summary
To be used in conjunction with the LM lequentlal mass properties Table 3.4-2)
Weight Amount Total
EVENT Consumable Change Remaining Usage
From To (Pounds) (Pounds) (Pounds)
Earth Orbit CSM/LM Separation D/S-Oxygen -1.1 46.9 -1.1
D/S-Water -i 3.0 2 37.0 -13.0
LM-RCS -5.0 600.0 -5.0
CSM/LM Pre P .D .I. D/S-Oxygen -I.0 45.9 -2. i
Separation D/S-Water -21.3 215.7 -34.3
LM-I_ S -55.5 545. i -60.5
Pre P.D.I. LM @ Touchdown D/S-Oxygen -0.i 45.8 -2.2
D/S-Water -I.I 214.6 -35.4
LM-I_S -97.0 448.1 -157.5
LM-DPS 17,332.5 989.1 17,332.5
A/S @ Touchdown A/S at Lift-Off LM-RCS -5.0 443.1 -162.5
A/S @ Llft-Off A/S in Orbit LM-APS 4931.1 279.9 4931.1
A/S in Orbit Pre T.P.I. A/S-Water -5.0 80.0 -5.0
A/S-Oxygen -0.3 4.5 -0.3
LM- RCS -47.4 395.7 209.9
Pre T.P.I. Post T.P.I. LM-APS 56.9 223.0 4988.0
A/S @ Post T.P.I. A/S @ Docking A/S-Water -3.8 76.2 -8.8
A/S-Oxygen -0.2 4.3 -0.5
LM-RC S 70.2 325.5 -280.1
A/S @ Docking A/S Jettison A/S-Water -8.2 68.0 -17.0
A/S-Oxygen -0.4 3.9 -0.9
NOTE :
Tanked LM RCS Propellant should be reduced by 0.3 ib
0.7 ib oxidizer.
fuel and
3.4-23
SNA-8-D-027(III) KEV 2