Maneuver Plan Plan Date (UTCG): 2009 271 13:47:04 Burn Start (UTCG): 2009 269 17:55:25.6 Pre-burn fuel mass (kg): 247.512 official Maneuver: MOI3 Burn Stop (UTCG): 2009 269 17:56:47.2 Post-burn fuel mass (kg): 244.587 official Planned dV (m/s): 5.095 Duration (s): 81.6 Fuel mass used (kg): 2.925 official Average SC Mass (kg): 1266.920 official Notes: MOI3 Calibration Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_MOI3_RECON_2009269_175500.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 1 270.200 20.0 NT2 2 270.200 20.0 NT3 1 270.200 20.0 NT4 2 270.200 20.0 AT1 1 270.200 20.0 230.661 16.474 1.003120 16.525 67 AT2 2 270.200 20.0 AT3 1 270.200 20.0 232.371 21.563 1.003120 21.630 88 AT4 2 270.200 20.0 AT5 1 270.200 20.0 233.574 24.435 1.003120 24.511 100 AT6 2 270.200 20.0 AT7 1 270.200 20.0 231.563 19.147 1.003120 19.207 78 AT8 2 270.200 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 270.200 20.0 NT2 2 270.200 20.0 NT3 1 270.200 20.0 NT4 2 270.200 20.0 AT1 1 270.200 20.0 230.661 16.474 1.003120 16.525 67 AT2 2 270.200 20.0 AT3 1 270.200 20.0 232.371 21.563 1.003120 21.630 88 AT4 2 270.200 20.0 AT5 1 270.200 20.0 233.574 24.435 1.003120 24.511 100 AT6 2 270.200 20.0 AT7 1 270.200 20.0 231.563 19.147 1.003120 19.207 78 AT8 2 270.200 20.0