5 - 24 TABLE 5-7 (CONT‘D) a These weights were used for analysis only and do not reflect the actual weight after consumables loading. b RCS propellant remaining of total loaded. LM-RCS PROPELLANT BUDGET TIME (HR) EVENT S/C WT (LBS) S/C RCS USED (LBS) S/C RCS LEFT (LBS) S/C RCS LEFT (%) .0 .0 .0 .9 .4 1.8 3.3 1.3 .4 .4 .4 .4 2.7 1.3 33.6 3.3 .4 1.3 4.1 .4 2.0 1.3 4.0 4.0 1.3 17.0 1.3 33.9 16.0 10.0 527.5 527.5 527.5 526.7 526.2 524.4 521.2 519.9 519.5 519.0 518.6 518.1 515.5 514.2 480.6 477.2 476.8 475.5 471.4 471.0 469.0 467.7 463.7 459.7 458.4 441.4 440.1 406.3 390.3 380.3 83.3 83.3 83.3 83.2 83.1 82.8 82.3 82.1 82.1 82.0 81.9 81.9 81.4 81.2 75.9 75.4 75.3 75.1 74.5 74.4 74.1 73.9 73.3 72.6 72.4 69.7 69.5 64.2 61.7 60.1 (a) (b) (b) 16580. 10840. 6087. 5969. 5969. 5967. 5964. 5962. 5962. 5961. 5961. 5961. 5958. 5957. 5923. 5920. 5919. 5918. 5914. 5913. 5911. 5910. 5906. 5902. 5901. 5884. 5883. 5849. 5833. 5823. ADD LUNAR SAMPLES LUNAR LIFT OFF POWERED ASCENT PHASE WITH RCS/APS INTERCONNECT POWERED ASCENT PHASE WITHOUT RCS/APS INTERCONNECT RR LOCK ON MNVR INSERTION BURN CONTROL TRIM OUT OF PLANE ERROR ATTITUDE HOLD IMU REALIHN STAR 1 IMU REALIHN STAR 2 IMU REALIHN STAR 3 RR LOCK ON MNVR MAINTAIN LOS ATTITUDE HOLD CSI BURN RCS +2 MAINTAIN LOS MNVR TO PLANE CHANGE ATTITUDE ATTITUDE HOLD RCS PLANE CHANGE BURN RR LOCK ON MNVR MAINTAIN LOS ATTITUDE HOLD CDH RCS BURN MAINTAIN LOS ATTITUDE HOLD RCS TPI BURN MAINTIN LOS MCC AND BRAKING ATTITUDE AND LOS CONTROL LM CONTROL CSM ACTIVE DOCKING 112 40 124 23 124 23 124 23 124 25 124 30 124 30 124 30 124 37 124 37 124 37 124 55 124 55 125 15 125 21 125 26 125 44 125 45 125 50 126 00 126 00 126 15 126 19 126 19 126 53 126 58 126 58 127 36 127 36 128 00