Maneuver Plan Plan Date (UTCG): 2009 233 13:54:14 Burn Start (UTCG): 2009 231 22:15:00.3 Pre-burn fuel mass (kg): 268.249 official Maneuver: MOI9 Burn Stop (UTCG): 2009 231 22:15:23.1 Post-burn fuel mass (kg): 267.432 official Planned dV (m/s): 1.383 Duration (s): 22.8 Fuel mass used (kg): 0.817 official Average SC Mass (kg): 1288.710 official Notes: BSR dV Calibration | States 540 & 549 Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_BSR_CAL_2009231_221500.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 1 271.100 20.0 NT2 2 271.100 20.0 NT3 1 271.100 20.0 NT4 2 271.100 20.0 AT1 1 271.100 20.0 230.756 16.762 0.991944 16.626 68 AT2 2 271.100 20.0 AT3 1 271.100 20.0 232.294 21.379 0.991944 21.206 87 AT4 2 271.100 20.0 AT5 1 271.100 20.0 233.580 24.499 0.991944 24.302 100 AT6 2 271.100 20.0 AT7 1 271.100 20.0 231.491 18.955 0.991944 18.802 77 AT8 2 271.100 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 271.100 20.0 NT2 2 271.100 20.0 NT3 1 271.100 20.0 NT4 2 271.100 20.0 AT1 1 271.100 20.0 230.756 16.762 0.991944 16.626 68 AT2 2 271.100 20.0 AT3 1 271.100 20.0 232.294 21.379 0.991944 21.206 87 AT4 2 271.100 20.0 AT5 1 271.100 20.0 233.580 24.499 0.991944 24.302 100 AT6 2 271.100 20.0 AT7 1 271.100 20.0 231.491 18.955 0.991944 18.802 77 AT8 2 271.100 20.0