5 - 3 TABLE 5-2 (a) Spacecraft weights are approximate and are included for reference only. (b) Note: These refer to usable SM RCS propellant. SM-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 1.7 3.2 3.2 3.2 3.2 3.2 3.5 4.2 4.5 4.5 4.5 4.5 4.5 4.5 4.5 5.5 5.9 MISSION G INITIALIZE PROP LOADING SM RCS CHECKOUT TRANSPOSITION AND DOCKING +X 0.8 FPS -X 0.3 FPS PITCH TO ACQUIRE S-IVB PITCH 180 DEG AT 1.5 DEG/SEC ROLL CSM 60 DEG 2 DEG/SEC NULL RELATIVE DEL V 0.5 FPS INDEX AND DOCK LM EJECTION -X 5 SEC 4 JET SPS BURN TO EVADE S-IVB ORIENT AT 0.2 DEG/SEC ATTITUDE HOLD 0.5 DEG DB PGNCS START TRANSIENT CONTROL SPS BURN BUILD UP STEADY STATE BURN TAILOFF DAMP SHUTDOWN TRANSIENT P52 IMU ALIGN NAVIGATION SIGHTINGS ORIENT AT 0.2 DEG/SEC 63457. 63457. 63451. 63445. 63443. 63440. 63439. 63435. 63409. 96717. 96712. 96712. 96710. 96707. 96508. 96467. 96466. 96466. 96461. .0 .0 5.8 6.1 2.4 2.3 1.3 4.0 26.0 7.4 4.4 .8 1.3 .0 .3 .7 1.1 .2 4.4 1220.0 1220.0 1214.2 1208.1 1205.7 1203.4 1202.1 1198.1 1172.1 1164.6 1160.2 1159.4 1158.1 1158.1 1157.8 1157.2 1156.1 1155.9 1151.5 100. 100. 100. 99. 99. 99. 99. 98. 96. 95. 95. 95. 95. 95. 95. 95. 95. 95. 94. (a) (b) (b)