Maneuver Plan Plan Date (UTCG): 2010 152 18:35:52 Burn Start (UTCG): 2010 150 16:25:06.0 Pre-burn fuel mass (kg): 191.905 official Maneuver: SK10a Burn Stop (UTCG): 2010 150 16:26:29.6 Post-burn fuel mass (kg): 188.906 official Planned dV (m/s): 5.362 Duration (s): 83.6 Fuel mass used (kg): 2.999 official Average SC Mass (kg): 1211.280 official Notes: SK10a Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK10a_RECON_2010150_162000.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 1 273.500 20.0 NT2 2 273.500 20.0 NT3 1 273.500 20.0 NT4 2 273.500 20.0 AT1 1 273.500 20.0 230.595 16.387 0.984684 16.136 66 AT2 2 273.500 20.0 AT3 1 273.500 20.0 232.396 21.772 0.984684 21.438 88 AT4 2 273.500 20.0 AT5 1 273.500 20.0 233.598 24.671 0.984684 24.293 100 AT6 2 273.500 20.0 AT7 1 273.500 20.0 231.430 18.843 0.984684 18.554 76 AT8 2 273.500 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 273.500 20.0 NT2 2 273.500 20.0 NT3 1 273.500 20.0 NT4 2 273.500 20.0 AT1 1 273.500 20.0 230.595 16.387 0.984684 16.136 66 AT2 2 273.500 20.0 AT3 1 273.500 20.0 232.396 21.772 0.984684 21.438 88 AT4 2 273.500 20.0 AT5 1 273.500 20.0 233.598 24.671 0.984684 24.293 100 AT6 2 273.500 20.0 AT7 1 273.500 20.0 231.430 18.843 0.984684 18.554 76 AT8 2 273.500 20.0