Maneuver Plan Plan Date (UTCG): 2010 260 14:01:31 Burn Start (UTCG): 2010 259 18:15:39.5 Pre-burn fuel mass (kg): 167.315 official Maneuver: SK14a Burn Stop (UTCG): 2010 259 18:17:09.7 Post-burn fuel mass (kg): 164.070 official Planned dV (m/s): 5.887 Duration (s): 90.2 Fuel mass used (kg): 3.245 official Average SC Mass (kg): 1186.560 official Notes: SK14a Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK14a_RECON_2010259_181039.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 20.0 230.502 16.140 0.978717 15.797 65 AT2 2 273.500 20.0 AT3 1 273.500 20.0 232.567 22.258 0.978717 21.784 90 AT4 2 273.500 20.0 AT5 1 273.500 20.0 233.598 24.671 0.978717 24.146 100 AT6 2 273.500 20.0 AT7 1 273.500 20.0 231.430 18.843 0.978717 18.442 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 20.0 230.502 16.140 0.978717 15.797 65 AT2 2 273.500 20.0 AT3 1 273.500 20.0 232.567 22.258 0.978717 21.784 90 AT4 2 273.500 20.0 AT5 1 273.500 20.0 233.598 24.671 0.978717 24.146 100 AT6 2 273.500 20.0 AT7 1 273.500 20.0 231.430 18.843 0.978717 18.442 76 AT8 2 273.500 20.0