Maneuver Plan Plan Date (UTCG): 2011 334 14:46:00 Burn Start (UTCG): 2011 331 16:44:58.9 Pre-burn fuel mass (kg): 67.171 official Maneuver: SK30b Burn Stop (UTCG): 2011 331 16:45:26.7 Post-burn fuel mass (kg): 66.195 official Planned dV (m/s): 1.921 Duration (s): 27.8 Fuel mass used (kg): 0.975 official Average SC Mass (kg): 1087.555 official Notes: SK30b Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK30b_RECON_2011331_163959.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 1 273.000 20.0 NT2 2 273.000 20.0 NT3 1 273.000 20.0 NT4 2 273.000 20.0 AT1 1 273.000 20.0 230.203 15.378 0.974309 14.983 62 AT2 2 273.000 20.0 AT3 1 273.000 20.0 232.392 21.740 0.974309 21.182 88 AT4 2 273.000 20.0 AT5 1 273.000 20.0 233.594 24.635 0.974309 24.002 100 AT6 2 273.000 20.0 AT7 1 273.000 20.0 231.187 18.081 0.974309 17.617 73 AT8 2 273.000 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 273.000 20.0 NT2 2 273.000 20.0 NT3 1 273.000 20.0 NT4 2 273.000 20.0 AT1 1 273.000 20.0 230.203 15.378 0.974309 14.983 62 AT2 2 273.000 20.0 AT3 1 273.000 20.0 232.392 21.740 0.974309 21.182 88 AT4 2 273.000 20.0 AT5 1 273.000 20.0 233.594 24.635 0.974309 24.002 100 AT6 2 273.000 20.0 AT7 1 273.000 20.0 231.187 18.081 0.974309 17.617 73 AT8 2 273.000 20.0