Maneuver Plan Plan Date (UTCG): 2009 327 19:41:29 Burn Start (UTCG): 2009 324 14:05:08.1 Pre-burn fuel mass (kg): 236.908 official Maneuver: SK03a Burn Stop (UTCG): 2009 324 14:06:30.7 Post-burn fuel mass (kg): 233.943 official Planned dV (m/s): 5.199 Duration (s): 82.6 Fuel mass used (kg): 2.965 official Average SC Mass (kg): 1256.295 official Notes: SK03a Calibration Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_SK03a_RECON_2009324_140508.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 1 272.700 20.0 NT2 2 272.700 20.0 NT3 1 272.700 20.0 NT4 2 272.700 20.0 AT1 1 272.700 20.0 230.589 16.349 1.001400 16.372 66 AT2 2 272.700 20.0 AT3 1 272.700 20.0 232.390 21.721 1.001400 21.752 88 AT4 2 272.700 20.0 AT5 1 272.700 20.0 233.592 24.614 1.001400 24.648 100 AT6 2 272.700 20.0 AT7 1 272.700 20.0 231.503 19.044 1.001400 19.070 77 AT8 2 272.700 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 272.700 20.0 NT2 2 272.700 20.0 NT3 1 272.700 20.0 NT4 2 272.700 20.0 AT1 1 272.700 20.0 230.589 16.349 1.001400 16.372 66 AT2 2 272.700 20.0 AT3 1 272.700 20.0 232.390 21.721 1.001400 21.752 88 AT4 2 272.700 20.0 AT5 1 272.700 20.0 233.592 24.614 1.001400 24.648 100 AT6 2 272.700 20.0 AT7 1 272.700 20.0 231.503 19.044 1.001400 19.070 77 AT8 2 272.700 20.0