Maneuver Plan Plan Date (UTCG): 2009 281 18:42:46 Burn Start (UTCG): 2009 280 19:15:00.7 Pre-burn fuel mass (kg): 244.477 official Maneuver: MOI4 Burn Stop (UTCG): 2009 280 19:15:10.1 Post-burn fuel mass (kg): 244.139 official Planned dV (m/s): 0.567 Duration (s): 9.4 Fuel mass used (kg): 0.338 official Average SC Mass (kg): 1265.180 official Notes: LPM (MOI4) Calibration - 3.6% Cold Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_MOI4_RECON_2009280_191500.a Maneuver Configuration: Bank 1 2 NT OFF OFF Prop Mode: PressureReg ACS Off-Pulsed OFF ACS Stop Mode: Time Initial Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 271.700 20.0 NT2 2 271.700 20.0 NT3 1 271.700 20.0 NT4 2 271.700 20.0 AT1 1 271.700 20.0 230.672 16.546 0.964282 15.955 67 AT2 2 271.700 20.0 AT3 1 271.700 20.0 232.383 21.658 0.964282 20.885 88 AT4 2 271.700 20.0 AT5 1 271.700 20.0 233.585 24.542 0.964282 23.666 100 AT6 2 271.700 20.0 AT7 1 271.700 20.0 231.574 19.232 0.964282 18.545 78 AT8 2 271.700 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 271.700 20.0 NT2 2 271.700 20.0 NT3 1 271.700 20.0 NT4 2 271.700 20.0 AT1 1 271.700 20.0 230.672 16.546 0.964282 15.955 67 AT2 2 271.700 20.0 AT3 1 271.700 20.0 232.383 21.658 0.964282 20.885 88 AT4 2 271.700 20.0 AT5 1 271.700 20.0 233.585 24.542 0.964282 23.666 100 AT6 2 271.700 20.0 AT7 1 271.700 20.0 231.574 19.232 0.964282 18.545 78 AT8 2 271.700 20.0