2 - 9 P30 MANEUVER PURPOSE XXXXX TYPE OF MNVR TO BE PERFORMED PROP/GUID XXX/XXX PROPULSION SYSTEM (SPS/RCS) GUIDANCE (SCS/G&N) WT +XXXXX (lbs) PREMANEUVER VEHICLE WEIGHT P TRIM ±X.XX (DEG) SPS PITCH GIMBAL OFFSET TO PLACE THRUST THROUGH THE CG Y TRIM ±X.XX (DEG) SPS YAW GIMBAL OFFSET TO PLACE THRUST THROUGH THE CG GETI XX:XX:XX.XX TIME OF MNVR IGNITION (HRS:MIN:SEC) ∆VX ±XXXX.X (FPS) P30 VELOCITY TO BE GAINED ∆VY ±XXXX.X (FPS) COMPONENTS IN LOCAL VERTICAL ∆VZ ±XXXX.X (FPS) COORDINATES R XXX (DEG) IMU GIMBAL ANGLES OF MANEUVER P XXX (DEG) ATTITUDE Y XXX (DEG) HA XXXX.X (NM) PREDICTED APOGEE ALTITUDE AFTER MANEUVER HP ±XXXX.X (NM) PREDICTED PERIGEE ALTITUDE AFTER MANEUVER ∆VT +XXXX.X (FPS) TOTAL VELOCITY OF MANEUVER BT X:XX (MIN:SEC) MANEUVER DURATION ∆VC XXXX.X (FPS) PREMANEUVER ∆V SETTING IN EMS ∆V COUNTER SXTS XX (OCTAL) SEXTANT STAR FOR MANEUVER ATTITUDE CK SFT +XXX.X (DEG) SEXTANT SHAFT SETTING FOR MANEUVER ATTITUDE CK TRN +XX.X (DEG) SEXTANT TRUNNION SETTING FOR MANEUVER ATTITUDE CK BSS XX (OCTAL) BORESIGHT STAR FOR MANEUVER ATTITUDE CK USING THE COAS SPA ±XX.X (DEG) BSS PITCH ANGLE ON COAS FOR MANEUVER ATTITUDE CK