Maneuver Plan Plan Date (UTCG): 2011 251 18:29:42 Burn Start (UTCG): 2011 249 17:16:16.5 Pre-burn fuel mass (kg): 85.491 official Maneuver: SK27a Burn Stop (UTCG): 2011 249 17:16:55.5 Post-burn fuel mass (kg): 84.109 official Planned dV (m/s): 2.713 Duration (s): 39.0 Fuel mass used (kg): 1.383 official Average SC Mass (kg): 1105.670 official Notes: SK27a Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK27a_RECON_2011249_171116.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 0.986623 15.442 63 AT2 2 273.600 20.0 AT3 1 273.600 20.0 232.482 22.021 0.986623 21.727 89 AT4 2 273.600 20.0 AT5 1 273.600 20.0 233.598 24.678 0.986623 24.348 100 AT6 2 273.600 20.0 AT7 1 273.600 20.0 231.272 18.358 0.986623 18.113 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 0.986623 15.442 63 AT2 2 273.600 20.0 AT3 1 273.600 20.0 232.482 22.021 0.986623 21.727 89 AT4 2 273.600 20.0 AT5 1 273.600 20.0 233.598 24.678 0.986623 24.348 100 AT6 2 273.600 20.0 AT7 1 273.600 20.0 231.272 18.358 0.986623 18.113 74 AT8 2 273.600 20.0