FLIGHT PLAN MCC-H NOTES MISSION PAGE DAY / REV TIME DATE EDITION APOLLO 11 3-5 1 / TLC 04:00 - 05:00 JULY 1, 1969 FINAL MSC Form 29 (May 69) FLIGHT PLANNING BRANCH 1330 EDT 04:00 :10 :20 :30 :40 :50 05:00 M S F N RECORD EVASIVE MNVR PAD GO/NO-GO FOR PYRO ARM & LM EJECTION DAP - R1 = 21101, R2 = 11111 PYRO LOGIC ARM THRUST MONITOR - P47 EXT ∆V = P30 DAP - R1 = 21111, R2 = 11111 DAP CONFIGURATION AFTER LM EJECTION SAME AS ABOVE EXCEPT CHANGE TO 5° DB PITCH DOWN 75° WRT LOCAL HORIZONTAL ROLL TO VISUALLY ACQ SIV-B SPS THRUST - P40 GDC ALIGN TO IMU SM RCS MON CK SM RCS MON CK SPS MON CK BURN STATUS REPORT V66 - TRANS CSM STATE VECTOR TO LM SLOT MANEUVER TO OBSERVE SLINGSHOT GETI = 04:09:45 BT = 3 SEC ∆VT = LM EJECTION GETI = 04:39:45 NO ULLAGE BT = 2.8 SEC ∆VT = 19.7 IN PLANE EVASIVE MNVR FOR LM EJECTION RELATIVE ∆V FROM SPRINGS = 1 FPS X X XXX XXX XX X XX X XXX XXX XX ∆TIG BT Vgx TRIM R P Y Vgx Vgy Vgz ∆Vc FUEL OX UNBAL BURN STATUS REPORT FIRST SPS BURN WILL ALWAYS START ON BANK A AND BANK B WILL BE ACTIVATED IF THE BURN 5 SEC DAP CONFIGURATION FOR LM EJECTION: CSM & LM 0.5° DB, .5°/SEC, A/C ROLL, 4 JETS NOTE: WITH RT TLM, ONLY ITEMS NORMALLY REQUIRED IN BURN STATUS REPORT ARE %VC, FUEL, OX, AND UNBAL EVASIVE MNVR GO/NO-GO UPDATE TLI CUT OFF + 1 HR 50 MIN