Maneuver Plan Plan Date (UTCG): 2011 347 15:54:58 Burn Start (UTCG): 2011 345 13:00:20.2 Pre-burn fuel mass (kg): 66.141 official Maneuver: SK31a Burn Stop (UTCG): 2011 345 13:07:43.6 Post-burn fuel mass (kg): 50.717 official Planned dV (m/s): 31.006 Duration (s): 443.4 Fuel mass used (kg): 15.423 official Average SC Mass (kg): 1079.300 official Notes: SK31a Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK31a_RECON_2011345_125520.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 1 271.100 20.0 NT2 2 271.100 20.0 NT3 1 271.100 20.0 NT4 2 271.100 20.0 AT1 1 271.100 20.0 230.189 15.293 0.987012 15.094 62 AT2 2 271.100 20.0 AT3 1 271.100 20.0 232.378 21.620 0.987012 21.339 88 AT4 2 271.100 20.0 AT5 1 271.100 20.0 233.580 24.499 0.987012 24.181 100 AT6 2 271.100 20.0 AT7 1 271.100 20.0 231.092 17.738 0.987012 17.507 72 AT8 2 271.100 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 271.100 20.0 NT2 2 271.100 20.0 NT3 1 271.100 20.0 NT4 2 271.100 20.0 AT1 1 271.100 20.0 230.189 15.293 0.987012 15.094 62 AT2 2 271.100 20.0 AT3 1 271.100 20.0 232.378 21.620 0.987012 21.339 88 AT4 2 271.100 20.0 AT5 1 271.100 20.0 233.580 24.499 0.987012 24.181 100 AT6 2 271.100 20.0 AT7 1 271.100 20.0 231.092 17.738 0.987012 17.507 72 AT8 2 271.100 20.0