Maneuver Plan Plan Date (UTCG): 2010 047 13:48:23 Burn Start (UTCG): 2010 040 15:24:28.4 Pre-burn fuel mass (kg): 217.725 official Maneuver: SK06a Burn Stop (UTCG): 2010 040 15:25:52.4 Post-burn fuel mass (kg): 214.717 official Planned dV (m/s): 5.317 Duration (s): 84.0 Fuel mass used (kg): 3.008 official Average SC Mass (kg): 1237.095 official Notes: SK06a Calibration Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_SK06a_RECON_2010040_151928.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 1 271.900 20.0 NT2 2 271.900 20.0 NT3 1 271.900 20.0 NT4 2 271.900 20.0 AT1 1 271.900 20.0 230.583 16.311 0.994077 16.214 66 AT2 2 271.900 20.0 AT3 1 271.900 20.0 232.384 21.671 0.994077 21.542 88 AT4 2 271.900 20.0 AT5 1 271.900 20.0 233.586 24.557 0.994077 24.411 100 AT6 2 271.900 20.0 AT7 1 271.900 20.0 231.497 18.999 0.994077 18.887 77 AT8 2 271.900 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 271.900 20.0 NT2 2 271.900 20.0 NT3 1 271.900 20.0 NT4 2 271.900 20.0 AT1 1 271.900 20.0 230.583 16.311 0.994077 16.214 66 AT2 2 271.900 20.0 AT3 1 271.900 20.0 232.384 21.671 0.994077 21.542 88 AT4 2 271.900 20.0 AT5 1 271.900 20.0 233.586 24.557 0.994077 24.411 100 AT6 2 271.900 20.0 AT7 1 271.900 20.0 231.497 18.999 0.994077 18.887 77 AT8 2 271.900 20.0