Maneuver Plan Plan Date (UTCG): 2010 260 14:02:20 Burn Start (UTCG): 2010 259 21:10:23.7 Pre-burn fuel mass (kg): 164.070 official Maneuver: SK14b Burn Stop (UTCG): 2010 259 21:11:46.5 Post-burn fuel mass (kg): 161.113 official Planned dV (m/s): 5.377 Duration (s): 82.8 Fuel mass used (kg): 2.957 official Average SC Mass (kg): 1183.460 official Notes: SK14b Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK14b_RECON_2010259_210523.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 20.0 230.498 16.117 0.978472 15.770 65 AT2 2 273.000 20.0 AT3 1 273.000 20.0 232.477 21.983 0.978472 21.510 89 AT4 2 273.000 20.0 AT5 1 273.000 20.0 233.594 24.635 0.978472 24.105 100 AT6 2 273.000 20.0 AT7 1 273.000 20.0 231.347 18.571 0.978472 18.171 75 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 20.0 230.498 16.117 0.978472 15.770 65 AT2 2 273.000 20.0 AT3 1 273.000 20.0 232.477 21.983 0.978472 21.510 89 AT4 2 273.000 20.0 AT5 1 273.000 20.0 233.594 24.635 0.978472 24.105 100 AT6 2 273.000 20.0 AT7 1 273.000 20.0 231.347 18.571 0.978472 18.171 75 AT8 2 273.000 20.0