Maneuver Plan Plan Date (UTCG): 2009 269 08:42:43 Burn Start (UTCG): 2009 268 18:27:56.8 Pre-burn fuel mass (kg): 250.811 official Maneuver: MOI2 Burn Stop (UTCG): 2009 268 18:29:28.8 Post-burn fuel mass (kg): 247.512 official Planned dV (m/s): 5.776 Duration (s): 92.0 Fuel mass used (kg): 3.299 official Average SC Mass (kg): 1270.030 official Notes: MOI2 CALIBRATION Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_MOI2_RECON_2009268_182756.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 1 271.300 20.0 NT2 2 271.300 20.0 NT3 1 271.300 20.0 NT4 2 271.300 20.0 AT1 1 271.300 20.0 230.669 16.527 1.011050 16.709 67 AT2 2 271.300 20.0 AT3 1 271.300 20.0 232.380 21.633 1.011050 21.872 88 AT4 2 271.300 20.0 AT5 1 271.300 20.0 233.582 24.514 1.011050 24.785 100 AT6 2 271.300 20.0 AT7 1 271.300 20.0 231.493 18.966 1.011050 19.176 77 AT8 2 271.300 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 271.300 20.0 NT2 2 271.300 20.0 NT3 1 271.300 20.0 NT4 2 271.300 20.0 AT1 1 271.300 20.0 230.669 16.527 1.011050 16.709 67 AT2 2 271.300 20.0 AT3 1 271.300 20.0 232.380 21.633 1.011050 21.872 88 AT4 2 271.300 20.0 AT5 1 271.300 20.0 233.582 24.514 1.011050 24.785 100 AT6 2 271.300 20.0 AT7 1 271.300 20.0 231.493 18.966 1.011050 19.176 77 AT8 2 271.300 20.0