Maneuver Plan Plan Date (UTCG): 2011 251 18:30:16 Burn Start (UTCG): 2011 249 20:32:52.5 Pre-burn fuel mass (kg): 84.109 official Maneuver: SK27b Burn Stop (UTCG): 2011 249 20:33:22.1 Post-burn fuel mass (kg): 83.059 official Planned dV (m/s): 2.039 Duration (s): 29.6 Fuel mass used (kg): 1.049 official Average SC Mass (kg): 1104.455 official Notes: SK27b Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK27b_RECON_2011249_202752.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 1 273.600 20.0 NT2 2 273.600 20.0 NT3 1 273.600 20.0 NT4 2 273.600 20.0 AT1 1 273.600 20.0 230.309 15.651 0.975863 15.274 63 AT2 2 273.600 20.0 AT3 1 273.600 20.0 232.482 22.021 0.975863 21.490 89 AT4 2 273.600 20.0 AT5 1 273.600 20.0 233.598 24.678 0.975863 24.083 100 AT6 2 273.600 20.0 AT7 1 273.600 20.0 231.272 18.358 0.975863 17.915 74 AT8 2 273.600 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 273.600 20.0 NT2 2 273.600 20.0 NT3 1 273.600 20.0 NT4 2 273.600 20.0 AT1 1 273.600 20.0 230.309 15.651 0.975863 15.274 63 AT2 2 273.600 20.0 AT3 1 273.600 20.0 232.482 22.021 0.975863 21.490 89 AT4 2 273.600 20.0 AT5 1 273.600 20.0 233.598 24.678 0.975863 24.083 100 AT6 2 273.600 20.0 AT7 1 273.600 20.0 231.272 18.358 0.975863 17.915 74 AT8 2 273.600 20.0