Maneuver Plan Plan Date (UTCG): 2010 007 16:06:37 Burn Start (UTCG): 2009 176 10:32:39.2 Pre-burn fuel mass (kg): 411.212 official Maneuver: LOI3 Burn Stop (UTCG): 2009 176 10:45:19.2 Post-burn fuel mass (kg): 343.982 official Planned dV (m/s): 110.723 Duration (s): 760.0 Fuel mass used (kg): 67.230 official Average SC Mass (kg): 1398.465 official Notes: UPDATE: LOI3 Calibration Report Ephemeris File Name: Thrust Vector File Name: S:\Products\STK Processed Att File\MOC68_LOI3_RECON_2009176_102739.a Maneuver Configuration: Bank 1 2 NT ON OFF Prop Mode: PressureReg ACS On-Pulsed On-Pulsed 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 1 268.650 20.0 232.120 93.750 1.019880 95.614 100 NT2 2 268.650 20.0 NT3 1 268.650 20.0 232.120 93.750 1.019880 95.614 100 NT4 2 268.650 20.0 AT1 1 268.650 20.0 209.136 1.827 1.019880 1.863 8 AT2 2 268.650 20.0 200.662 0.000 1.019880 0.000 0 AT3 1 268.650 20.0 200.662 0.000 1.019880 0.000 0 AT4 2 268.650 20.0 200.662 0.000 1.019880 0.000 0 AT5 1 268.650 20.0 211.778 2.580 1.019880 2.631 11 AT6 2 268.650 20.0 211.778 2.580 1.019880 2.631 11 AT7 1 268.650 20.0 212.599 2.830 1.019880 2.887 12 AT8 2 268.650 20.0 212.599 2.830 1.019880 2.887 12 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 268.650 20.0 232.120 93.750 1.019880 95.614 100 NT2 2 268.650 20.0 NT3 1 268.650 20.0 232.120 93.750 1.019880 95.614 100 NT4 2 268.650 20.0 AT1 1 268.650 20.0 209.136 1.827 1.019880 1.863 8 AT2 2 268.650 20.0 200.662 0.000 1.019880 0.000 0 AT3 1 268.650 20.0 200.662 0.000 1.019880 0.000 0 AT4 2 268.650 20.0 200.662 0.000 1.019880 0.000 0 AT5 1 268.650 20.0 211.778 2.580 1.019880 2.631 11 AT6 2 268.650 20.0 211.778 2.580 1.019880 2.631 11 AT7 1 268.650 20.0 212.599 2.830 1.019880 2.887 12 AT8 2 268.650 20.0 212.599 2.830 1.019880 2.887 12