Apollo 11 Flight Plan, Final - July 1, 1969 Page 68 (68 of 353)

2 - 20 RETDRO XX:XX TIME FROM EI TO DROGUE DEPLOY (MIN:SEC) SXTS XX (OCTAL) SEXTANT STAR FOR ENTRY ATTITUDE CHECK SFT +XXX. X (DEG) SEXTANT SHAFT SETTING FOR ENTRY ATTITUDE CHECK TRN +XX. X (DEG) SEXTANT TRUNNION SETTING FOR ENTRY ATTITUDE CHECK BSS XXX (OCTAL) BORESIGHT STAR FOR ENTRY ATTITUDE CHECK USING THE COAS SPA ±XX.X (DEG) BSS PITCH ANGLE ON COAS FOR ENTRY ATTITUDE CHECK SXP ±X.X (DEG) BSS X POSITION ON COAS FOR ENTRY ATTITUDE CHECK LIFT VECTOR XX (UP/DN) LIFT VECTOR DESIRED AT .05G‘s BASED ON ENTRY CORRIDOR

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2 - 20 RETDRO XX:XX TIME FROM EI TO DROGUE DEPLOY (MIN:SEC) SXTS XX (OCTAL) SEXTANT STAR FOR ENTRY ATTITUDE CHECK SFT +XXX. X (DEG) SEXTANT SHAFT SETTING FOR ENTRY ATTITUDE CHECK TRN +XX. X (DEG) SEXTANT TRUNNION SETTING FOR ENTRY ATTITUDE CHECK BSS XXX (OCTAL) BORESIGHT STAR FOR ENTRY ATTITUDE CHECK USING THE COAS SPA ±XX.X (DEG) BSS PITCH ANGLE ON COAS FOR ENTRY ATTITUDE CHECK SXP ±X.X (DEG) BSS X POSITION ON COAS FOR ENTRY ATTITUDE CHECK LIFT VECTOR XX (UP/DN) LIFT VECTOR DESIRED AT .05G‘s BASED ON ENTRY CORRIDOR

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2 - 19 LUNAR ENTRY PAD AREA XXXXX SPLASHDOWN AREA DEFINED BY TARGET LINE R .05G XXX (DEG) SPACECRAFT IMU GIMBAL ANGLES P .05G XXX (DEG) REQUIRED FOR AERODYNAMIC TRIM Y .05G XXX (DEG) AT .05G GET XXX:XX:XX TIME OF ENTRY ATTITUDE HORIZ (HOR CK) (HRS:MIN:SEC) CHECK AT EI -17 MIN. P XXX (DEG) PITCH ATTITUDE FOR HORIZON CHECK (HOR CK) AT EI -17 MIN. LAT ±XX.XX (DEG) LATITUDE OF TARGET POINT LONG ±XXX.XX (DEG) LONGITUDE OF TARGET POINT MAX G XX.X (G‘s) PREDICTED MAXIMUM REENTRY ACCELERATION V400K +XXXXX (FPS) INERTIAL VELOCITY AT ENTRY INTERFACE γ400K -X.XX (DEG) INERTIAL FLIGHT PATH ANGLE AT ENTRY INTERFACE RTGO +XXXX.X (NM) RANGE TO GO FROM .05G TO TARGET FOR EMS INITIALIZATION VI0 +XXXXX (fps) INERTIAL VELOCITY AT .05G FOR EMS INITIALIZATION RRT XXX:XX:XX REENTRY REFERENCE TIME BASED ON (HRS:MIN:SEC) GET OF PREDICTED 400K (GET START) RET .05G XX:XX TIME OF .05G FROM 400K (RRT) (MIN:SEC) DL MAX +X.XX (G‘s) MAXIMUM ACCEPTABLE VALUE OF PREDICTED DRAG LEVEL (FROM CMC) DL MIN +X.XX (G‘s) MINIMUM ACCEPTABLE VALUE OF PREDICTED DRAG LEVEL (FROM CMC) VL MAX +XXXXX (FPS) MAXIMUM ACCEPTABLE VALUE OF EXIT VELOCITY (FROM CMC) VL MIN +XXXXX (FPS) MINIMUM ACCEPTABLE VALUE OF EXIT VELOCITY (FROM CMC) DO X.XX (G‘s) PLANNED DRAG LEVEL DURING CONSTANT G RET VCIRC XX:XX TIME FROM EI THAT S/C VELOCITY (MIN:SEC) BECOMES CIRCULAR RETBBO XX:XX TIME FROM EI TO THE BEGINNING (MIN:SEC) OF BLACKOUT RETEBO XX:XX TIME FROM EI TO THE END OF (MIN:SEC) BLACKOUT

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Page 21Section I - General click to expand contents

Page 45Section II - Update Forms click to expand contents

Page 101Section III - Detailed Timeline click to expand contents

Page 1153. Translunar Coast Activities click to expand contents

Page 1734. Lunar Orbit Activities click to expand contents

Page 267Section IV - Detailed Test Objectives click to expand contents

Page 289Section V - Consumables click to expand contents

Apollo 11 Flight Plan, Final - July 1, 1969 resources

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Apollo 11 Flight Plan, Final - July 1, 1969 resources

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