Maneuver Plan Plan Date (UTCG): 2009 352 15:10:16 Burn Start (UTCG): 2009 351 21:08:23.3 Pre-burn fuel mass (kg): 227.314 official Maneuver: SK04b Burn Stop (UTCG): 2009 351 21:09:51.3 Post-burn fuel mass (kg): 224.170 official Planned dV (m/s): 5.531 Duration (s): 88.0 Fuel mass used (kg): 3.144 official Average SC Mass (kg): 1246.610 official Notes: SK04b Calibration Report Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_SK04b_RECON_2009351_210824.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 1 271.100 20.0 NT2 2 271.100 20.0 NT3 1 271.100 20.0 NT4 2 271.100 20.0 AT1 1 271.100 20.0 230.577 16.273 0.997001 16.224 66 AT2 2 271.100 20.0 AT3 1 271.100 20.0 232.378 21.620 0.997001 21.555 88 AT4 2 271.100 20.0 AT5 1 271.100 20.0 233.580 24.499 0.997001 24.426 100 AT6 2 271.100 20.0 AT7 1 271.100 20.0 231.491 18.955 0.997001 18.898 77 AT8 2 271.100 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 271.100 20.0 NT2 2 271.100 20.0 NT3 1 271.100 20.0 NT4 2 271.100 20.0 AT1 1 271.100 20.0 230.577 16.273 0.997001 16.224 66 AT2 2 271.100 20.0 AT3 1 271.100 20.0 232.378 21.620 0.997001 21.555 88 AT4 2 271.100 20.0 AT5 1 271.100 20.0 233.580 24.499 0.997001 24.426 100 AT6 2 271.100 20.0 AT7 1 271.100 20.0 231.491 18.955 0.997001 18.898 77 AT8 2 271.100 20.0