Maneuver Plan Plan Date (UTCG): 2011 277 19:05:10 Burn Start (UTCG): 2011 276 17:48:34.8 Pre-burn fuel mass (kg): 82.796 official Maneuver: SK28a Burn Stop (UTCG): 2011 276 17:49:50.0 Post-burn fuel mass (kg): 80.136 official Planned dV (m/s): 5.189 Duration (s): 75.2 Fuel mass used (kg): 2.660 official Average SC Mass (kg): 1102.340 official Notes: SK28a Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK28a_RECON_2011276_174335.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 1 273.800 20.0 NT2 2 273.800 20.0 NT3 1 273.800 20.0 NT4 2 273.800 20.0 AT1 1 273.800 20.0 230.209 15.413 0.977874 15.072 62 AT2 2 273.800 20.0 AT3 1 273.800 20.0 232.483 22.034 0.977874 21.546 89 AT4 2 273.800 20.0 AT5 1 273.800 20.0 233.600 24.692 0.977874 24.146 100 AT6 2 273.800 20.0 AT7 1 273.800 20.0 231.273 18.369 0.977874 17.962 74 AT8 2 273.800 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 273.800 20.0 NT2 2 273.800 20.0 NT3 1 273.800 20.0 NT4 2 273.800 20.0 AT1 1 273.800 20.0 230.209 15.413 0.977874 15.072 62 AT2 2 273.800 20.0 AT3 1 273.800 20.0 232.483 22.034 0.977874 21.546 89 AT4 2 273.800 20.0 AT5 1 273.800 20.0 233.600 24.692 0.977874 24.146 100 AT6 2 273.800 20.0 AT7 1 273.800 20.0 231.273 18.369 0.977874 17.962 74 AT8 2 273.800 20.0