Maneuver Plan Plan Date (UTCG): 2010 014 14:37:09 Burn Start (UTCG): 2010 013 19:41:59.5 Pre-burn fuel mass (kg): 221.079 official Maneuver: SK05b Burn Stop (UTCG): 2010 013 19:43:26.3 Post-burn fuel mass (kg): 217.980 official Planned dV (m/s): 5.473 Duration (s): 86.8 Fuel mass used (kg): 3.099 official Average SC Mass (kg): 1240.400 official Notes: SK05b Calibration Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_SK05b_RECON_2010013_193659.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 1 270.800 20.0 NT2 2 270.800 20.0 NT3 1 270.800 20.0 NT4 2 270.800 20.0 AT1 1 270.800 20.0 230.575 16.258 0.996001 16.193 66 AT2 2 270.800 20.0 AT3 1 270.800 20.0 232.376 21.601 0.996001 21.515 88 AT4 2 270.800 20.0 AT5 1 270.800 20.0 233.578 24.478 0.996001 24.380 100 AT6 2 270.800 20.0 AT7 1 270.800 20.0 231.489 18.938 0.996001 18.863 77 AT8 2 270.800 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 270.800 20.0 NT2 2 270.800 20.0 NT3 1 270.800 20.0 NT4 2 270.800 20.0 AT1 1 270.800 20.0 230.575 16.258 0.996001 16.193 66 AT2 2 270.800 20.0 AT3 1 270.800 20.0 232.376 21.601 0.996001 21.515 88 AT4 2 270.800 20.0 AT5 1 270.800 20.0 233.578 24.478 0.996001 24.380 100 AT6 2 270.800 20.0 AT7 1 270.800 20.0 231.489 18.938 0.996001 18.863 77 AT8 2 270.800 20.0