Maneuver Plan Plan Date (UTCG): 2010 070 16:35:51 Burn Start (UTCG): 2010 068 17:22:28.3 Pre-burn fuel mass (kg): 208.225 official Maneuver: SK07b Burn Stop (UTCG): 2010 068 17:23:55.9 Post-burn fuel mass (kg): 205.092 official Planned dV (m/s): 5.573 Duration (s): 87.6 Fuel mass used (kg): 3.133 official Average SC Mass (kg): 1227.530 official Notes: SK07b Calibration Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_SK07b_RECON_2010068_171727.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 1 271.400 20.0 NT2 2 271.400 20.0 NT3 1 271.400 20.0 NT4 2 271.400 20.0 AT1 1 271.400 20.0 230.579 16.287 0.992779 16.169 66 AT2 2 271.400 20.0 AT3 1 271.400 20.0 232.380 21.639 0.992779 21.483 88 AT4 2 271.400 20.0 AT5 1 271.400 20.0 233.583 24.521 0.992779 24.344 100 AT6 2 271.400 20.0 AT7 1 271.400 20.0 231.493 18.972 0.992779 18.835 77 AT8 2 271.400 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 271.400 20.0 NT2 2 271.400 20.0 NT3 1 271.400 20.0 NT4 2 271.400 20.0 AT1 1 271.400 20.0 230.579 16.287 0.992779 16.169 66 AT2 2 271.400 20.0 AT3 1 271.400 20.0 232.380 21.639 0.992779 21.483 88 AT4 2 271.400 20.0 AT5 1 271.400 20.0 233.583 24.521 0.992779 24.344 100 AT6 2 271.400 20.0 AT7 1 271.400 20.0 231.493 18.972 0.992779 18.835 77 AT8 2 271.400 20.0