Maneuver Plan Plan Date (UTCG): 2010 014 14:36:21 Burn Start (UTCG): 2010 013 16:50:58.3 Pre-burn fuel mass (kg): 224.134 official Maneuver: SK05a Burn Stop (UTCG): 2010 013 16:52:23.7 Post-burn fuel mass (kg): 221.079 official Planned dV (m/s): 5.397 Duration (s): 85.4 Fuel mass used (kg): 3.055 official Average SC Mass (kg): 1243.475 official Notes: SK05a Calibration Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_SK05a_RECON_2010013_164558.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 1 271.500 20.0 NT2 2 271.500 20.0 NT3 1 271.500 20.0 NT4 2 271.500 20.0 AT1 1 271.500 20.0 230.580 16.292 0.998699 16.270 66 AT2 2 271.500 20.0 AT3 1 271.500 20.0 232.381 21.646 0.998699 21.617 88 AT4 2 271.500 20.0 AT5 1 271.500 20.0 233.583 24.528 0.998699 24.496 100 AT6 2 271.500 20.0 AT7 1 271.500 20.0 231.494 18.977 0.998699 18.953 77 AT8 2 271.500 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 271.500 20.0 NT2 2 271.500 20.0 NT3 1 271.500 20.0 NT4 2 271.500 20.0 AT1 1 271.500 20.0 230.580 16.292 0.998699 16.270 66 AT2 2 271.500 20.0 AT3 1 271.500 20.0 232.381 21.646 0.998699 21.617 88 AT4 2 271.500 20.0 AT5 1 271.500 20.0 233.583 24.528 0.998699 24.496 100 AT6 2 271.500 20.0 AT7 1 271.500 20.0 231.494 18.977 0.998699 18.953 77 AT8 2 271.500 20.0