Maneuver Plan Plan Date (UTCG): 2009 327 19:42:06 Burn Start (UTCG): 2009 324 16:54:53.9 Pre-burn fuel mass (kg): 233.943 official Maneuver: SK03b Burn Stop (UTCG): 2009 324 16:56:29.7 Post-burn fuel mass (kg): 230.520 official Planned dV (m/s): 5.998 Duration (s): 95.8 Fuel mass used (kg): 3.423 official Average SC Mass (kg): 1253.100 official Notes: SK03b Calibration Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_SK03b_RECON_2009324_165454.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 1 272.100 20.0 NT2 2 272.100 20.0 NT3 1 272.100 20.0 NT4 2 272.100 20.0 AT1 1 272.100 20.0 230.584 16.320 0.998363 16.293 66 AT2 2 272.100 20.0 AT3 1 272.100 20.0 232.301 21.441 0.998363 21.406 87 AT4 2 272.100 20.0 AT5 1 272.100 20.0 233.588 24.571 0.998363 24.531 100 AT6 2 272.100 20.0 AT7 1 272.100 20.0 231.498 19.011 0.998363 18.979 77 AT8 2 272.100 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 272.100 20.0 NT2 2 272.100 20.0 NT3 1 272.100 20.0 NT4 2 272.100 20.0 AT1 1 272.100 20.0 230.584 16.320 0.998363 16.293 66 AT2 2 272.100 20.0 AT3 1 272.100 20.0 232.301 21.441 0.998363 21.406 87 AT4 2 272.100 20.0 AT5 1 272.100 20.0 233.588 24.571 0.998363 24.531 100 AT6 2 272.100 20.0 AT7 1 272.100 20.0 231.498 19.011 0.998363 18.979 77 AT8 2 272.100 20.0