Maneuver Plan Plan Date (UTCG): 2009 299 16:28:16 Burn Start (UTCG): 2009 296 14:27:18.9 Pre-burn fuel mass (kg): 243.833 official Maneuver: SK02a Burn Stop (UTCG): 2009 296 14:28:47.5 Post-burn fuel mass (kg): 240.648 official Planned dV (m/s): 5.545 Duration (s): 88.6 Fuel mass used (kg): 3.185 official Average SC Mass (kg): 1263.110 official Notes: SK02a Calibration Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_SK02a_RECON_2009296_142219.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 1 272.200 20.0 NT2 2 272.200 20.0 NT3 1 272.200 20.0 NT4 2 272.200 20.0 AT1 1 272.200 20.0 230.676 16.570 0.999750 16.566 67 AT2 2 272.200 20.0 AT3 1 272.200 20.0 232.386 21.690 0.999750 21.684 88 AT4 2 272.200 20.0 AT5 1 272.200 20.0 233.588 24.578 0.999750 24.572 100 AT6 2 272.200 20.0 AT7 1 272.200 20.0 231.499 19.016 0.999750 19.011 77 AT8 2 272.200 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 272.200 20.0 NT2 2 272.200 20.0 NT3 1 272.200 20.0 NT4 2 272.200 20.0 AT1 1 272.200 20.0 230.676 16.570 0.999750 16.566 67 AT2 2 272.200 20.0 AT3 1 272.200 20.0 232.386 21.690 0.999750 21.684 88 AT4 2 272.200 20.0 AT5 1 272.200 20.0 233.588 24.578 0.999750 24.572 100 AT6 2 272.200 20.0 AT7 1 272.200 20.0 231.499 19.016 0.999750 19.011 77 AT8 2 272.200 20.0