Maneuver Plan Plan Date (UTCG): 2010 236 15:21:35 Burn Start (UTCG): 2010 232 12:18:46.5 Pre-burn fuel mass (kg): 173.589 official Maneuver: SK13a Burn Stop (UTCG): 2010 232 12:20:11.9 Post-burn fuel mass (kg): 170.527 official Planned dV (m/s): 5.554 Duration (s): 85.4 Fuel mass used (kg): 3.062 official Average SC Mass (kg): 1192.930 official Notes: SK13a Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK13a_RECON_2010232_121346.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 1 273.400 20.0 NT2 2 273.400 20.0 NT3 1 273.400 20.0 NT4 2 273.400 20.0 AT1 1 273.400 20.0 230.501 16.135 0.983539 15.870 65 AT2 2 273.400 20.0 AT3 1 273.400 20.0 232.480 22.009 0.983539 21.646 89 AT4 2 273.400 20.0 AT5 1 273.400 20.0 233.597 24.664 0.983539 24.258 100 AT6 2 273.400 20.0 AT7 1 273.400 20.0 231.429 18.838 0.983539 18.528 76 AT8 2 273.400 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 273.400 20.0 NT2 2 273.400 20.0 NT3 1 273.400 20.0 NT4 2 273.400 20.0 AT1 1 273.400 20.0 230.501 16.135 0.983539 15.870 65 AT2 2 273.400 20.0 AT3 1 273.400 20.0 232.480 22.009 0.983539 21.646 89 AT4 2 273.400 20.0 AT5 1 273.400 20.0 233.597 24.664 0.983539 24.258 100 AT6 2 273.400 20.0 AT7 1 273.400 20.0 231.429 18.838 0.983539 18.528 76 AT8 2 273.400 20.0