FLIGHT PLAN CMP MISSION PAGE DAY / REV TIME DATE EDITION APOLLO 11 3-67 5 / 13 100:00 - 101:00 JULY 1, 1969 FINAL MSC Form 2189 (OT) (Nov 68) FLIGHT PLANNING BRANCH 1330 EDT 100:00 100:19 100:30 100:48 100:54 101:00 CDR LMP CSM LM MCC-H M S F N M S F N CSM SEPARATION GET: 100:39:50 BT: 8.0 SEC ∆VT: 2.5 FPS -X THRUSTERS ORBIT: 55.6 x 63.1 RR TRANSPONDER ACT & SELF TEST CONFIGURE DAP FOR UNDOCKING, CSM ONLY R1 = 11102 R2 = 11111 SC CONT - SCS START 16mm CAMERA ENABLE B3 & C4 RCS JETS V64 ACQUIRE MSFN LM INSPECTION, CAMERA OFF COPY PADS SC CONT - CMC P30 EXT ∆V P41 RCS THRUST P20 AUTO MANEUVER SXT & VHF RANGING COPY PAD UNDOCK DAP DATA LOAD LR ACT AND SELF TEST CSM: R 0, P 90/14, Y 0 HGA P -46, Y 3 YAW LEFT 60°, PITCH UP 110° SET ORDEAL YAW 360°, LM INSPECTION DON HELMETS AND GLOVES PREPARE FOR UNDOCKING P30 EXT ∆V RR MAN LOCK - ON VHF RANGING RR - OFF UNDOCK SEPARATION LM FDAI: R 0, P 194, Y 60 LM FDAI: R 0, P 304, Y 0 ACQUIRE MSFN ANT P 123, Y -37 P27 UPDATE BIO MED SWITCH - LEFT COPY PADS P27 UPDATE V47 AGS UPDATE AGS ALIGN COPY PAD V47 AGS ALIGN CSM: R 0, P 15/14, Y 0 LM STATE VECTOR (DOI -10) DOI TARGET LOAD DESCENT TARGET LOAD PIPA BIAS UPLINK LGC DOI MNVR PAD PDI PAD PDI ABORT 10 MIN NO PDI +12 PAD PDI ABORT 10 MIN UPDATE LM CSM STATE VECTOR (PDI +25) UPLINK LGC LUNAR SURFACE PAD UPDATE LM CSM RESCUE PAD UPDATE CSM