Maneuver Plan Plan Date (UTCG): 2009 259 20:26:10 Burn Start (UTCG): 2009 258 19:32:25.7 Pre-burn fuel mass (kg): 267.141 official Maneuver: MOI1 Burn Stop (UTCG): 2009 258 19:35:29.7 Post-burn fuel mass (kg): 250.985 official Planned dV (m/s): 28.909 Duration (s): 184.0 Fuel mass used (kg): 16.156 official Average SC Mass (kg): 1279.930 official Notes: MOI1 CAL 1.3% hot (0.1% cold wrt plan) Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_MOI1_2009258_192700.a Maneuver Configuration: Bank 1 2 NT ON OFF Prop Mode: PressureReg ACS On-Pulsed On-Pulsed 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 1 269.750 20.0 232.157 94.099 1.012950 95.317 100 NT2 2 269.750 20.0 NT3 1 269.750 20.0 232.157 94.099 1.012950 95.317 100 NT4 2 269.750 20.0 AT1 1 269.750 20.0 202.998 0.318 1.012950 0.322 2 AT2 2 269.750 20.0 200.670 0.000 1.012950 0.000 0 AT3 1 269.750 20.0 200.670 0.000 1.012950 0.000 0 AT4 2 269.750 20.0 200.670 0.000 1.012950 0.000 0 AT5 1 269.750 20.0 212.608 2.840 1.012950 2.876 12 AT6 2 269.750 20.0 211.786 2.588 1.012950 2.622 11 AT7 1 269.750 20.0 211.786 2.588 1.012950 2.622 11 AT8 2 269.750 20.0 210.936 2.337 1.012950 2.367 10 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 269.750 20.0 232.157 94.099 1.012950 95.317 100 NT2 2 269.750 20.0 NT3 1 269.750 20.0 232.157 94.099 1.012950 95.317 100 NT4 2 269.750 20.0 AT1 1 269.750 20.0 202.998 0.318 1.012950 0.322 2 AT2 2 269.750 20.0 200.670 0.000 1.012950 0.000 0 AT3 1 269.750 20.0 200.670 0.000 1.012950 0.000 0 AT4 2 269.750 20.0 200.670 0.000 1.012950 0.000 0 AT5 1 269.750 20.0 212.608 2.840 1.012950 2.876 12 AT6 2 269.750 20.0 211.786 2.588 1.012950 2.622 11 AT7 1 269.750 20.0 211.786 2.588 1.012950 2.622 11 AT8 2 269.750 20.0 210.936 2.337 1.012950 2.367 10