Maneuver Plan Plan Date (UTCG): 2009 352 15:09:41 Burn Start (UTCG): 2009 351 18:16:08.3 Pre-burn fuel mass (kg): 230.375 official Maneuver: SK04a Burn Stop (UTCG): 2009 351 18:17:33.7 Post-burn fuel mass (kg): 227.314 official Planned dV (m/s): 5.366 Duration (s): 85.4 Fuel mass used (kg): 3.061 official Average SC Mass (kg): 1249.715 official Notes: SK04a Calibration Report Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_SK04a_RECON_2009351_181608.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 0.995916 16.258 66 AT2 2 272.200 20.0 AT3 1 272.200 20.0 232.386 21.690 0.995916 21.601 88 AT4 2 272.200 20.0 AT5 1 272.200 20.0 233.588 24.578 0.995916 24.478 100 AT6 2 272.200 20.0 AT7 1 272.200 20.0 231.499 19.016 0.995916 18.938 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 0.995916 16.258 66 AT2 2 272.200 20.0 AT3 1 272.200 20.0 232.386 21.690 0.995916 21.601 88 AT4 2 272.200 20.0 AT5 1 272.200 20.0 233.588 24.578 0.995916 24.478 100 AT6 2 272.200 20.0 AT7 1 272.200 20.0 231.499 19.016 0.995916 18.938 77 AT8 2 272.200 20.0