Maneuver Plan Plan Date (UTCG): 2011 347 15:55:26 Burn Start (UTCG): 2011 345 16:02:58.0 Pre-burn fuel mass (kg): 50.717 official Maneuver: SK31b Burn Stop (UTCG): 2011 345 16:03:27.8 Post-burn fuel mass (kg): 49.675 official Planned dV (m/s): 2.085 Duration (s): 29.8 Fuel mass used (kg): 1.042 official Average SC Mass (kg): 1071.070 official Notes: SK31b Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK31b_RECON_2011345_155758.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 1 271.800 20.0 NT2 2 271.800 20.0 NT3 1 271.800 20.0 NT4 2 271.800 20.0 AT1 1 271.800 20.0 230.195 15.324 0.975131 14.943 62 AT2 2 271.800 20.0 AT3 1 271.800 20.0 232.469 21.906 0.975131 21.362 89 AT4 2 271.800 20.0 AT5 1 271.800 20.0 233.585 24.550 0.975131 23.939 100 AT6 2 271.800 20.0 AT7 1 271.800 20.0 231.097 17.774 0.975131 17.332 72 AT8 2 271.800 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 271.800 20.0 NT2 2 271.800 20.0 NT3 1 271.800 20.0 NT4 2 271.800 20.0 AT1 1 271.800 20.0 230.195 15.324 0.975131 14.943 62 AT2 2 271.800 20.0 AT3 1 271.800 20.0 232.469 21.906 0.975131 21.362 89 AT4 2 271.800 20.0 AT5 1 271.800 20.0 233.585 24.550 0.975131 23.939 100 AT6 2 271.800 20.0 AT7 1 271.800 20.0 231.097 17.774 0.975131 17.332 72 AT8 2 271.800 20.0