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