Maneuver Plan Plan Date (UTCG): 2010 097 20:16:04 Burn Start (UTCG): 2010 095 19:48:21.4 Pre-burn fuel mass (kg): 201.746 official Maneuver: SK08b Burn Stop (UTCG): 2010 095 19:49:46.4 Post-burn fuel mass (kg): 198.699 official Planned dV (m/s): 5.431 Duration (s): 85.0 Fuel mass used (kg): 3.047 official Average SC Mass (kg): 1221.095 official Notes: SK08b Calibration Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_SK08b_RECON_2010095_194322.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 20.0 230.585 16.325 0.989548 16.154 66 AT2 2 272.200 20.0 AT3 1 272.200 20.0 232.386 21.690 0.989548 21.463 88 AT4 2 272.200 20.0 AT5 1 272.200 20.0 233.588 24.578 0.989548 24.321 100 AT6 2 272.200 20.0 AT7 1 272.200 20.0 231.499 19.016 0.989548 18.817 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 20.0 230.585 16.325 0.989548 16.154 66 AT2 2 272.200 20.0 AT3 1 272.200 20.0 232.386 21.690 0.989548 21.463 88 AT4 2 272.200 20.0 AT5 1 272.200 20.0 233.588 24.578 0.989548 24.321 100 AT6 2 272.200 20.0 AT7 1 272.200 20.0 231.499 19.016 0.989548 18.817 77 AT8 2 272.200 20.0