Maneuver Plan Plan Date (UTCG): 2010 097 20:15:27 Burn Start (UTCG): 2010 095 16:54:50.6 Pre-burn fuel mass (kg): 204.756 official Maneuver: SK08a Burn Stop (UTCG): 2010 095 16:56:14.2 Post-burn fuel mass (kg): 201.746 official Planned dV (m/s): 5.372 Duration (s): 83.6 Fuel mass used (kg): 3.010 official Average SC Mass (kg): 1224.125 official Notes: SK08a Calibration Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_SK08a_RECON_2010095_164951.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 1 272.800 20.0 NT2 2 272.800 20.0 NT3 1 272.800 20.0 NT4 2 272.800 20.0 AT1 1 272.800 20.0 230.589 16.353 0.992969 16.238 66 AT2 2 272.800 20.0 AT3 1 272.800 20.0 232.476 21.970 0.992969 21.816 89 AT4 2 272.800 20.0 AT5 1 272.800 20.0 233.593 24.621 0.992969 24.448 100 AT6 2 272.800 20.0 AT7 1 272.800 20.0 231.504 19.049 0.992969 18.915 77 AT8 2 272.800 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 272.800 20.0 NT2 2 272.800 20.0 NT3 1 272.800 20.0 NT4 2 272.800 20.0 AT1 1 272.800 20.0 230.589 16.353 0.992969 16.238 66 AT2 2 272.800 20.0 AT3 1 272.800 20.0 232.476 21.970 0.992969 21.816 89 AT4 2 272.800 20.0 AT5 1 272.800 20.0 233.593 24.621 0.992969 24.448 100 AT6 2 272.800 20.0 AT7 1 272.800 20.0 231.504 19.049 0.992969 18.915 77 AT8 2 272.800 20.0