Maneuver Plan Plan Date (UTCG): 2011 033 17:11:19 Burn Start (UTCG): 2011 031 20:36:20.5 Pre-burn fuel mass (kg): 136.605 official Maneuver: SK19a Burn Stop (UTCG): 2011 031 20:37:39.9 Post-burn fuel mass (kg): 133.776 official Planned dV (m/s): 5.258 Duration (s): 79.4 Fuel mass used (kg): 2.829 official Average SC Mass (kg): 1156.065 official Notes: SK19a CALIBRATION Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK19a_RECON_2011031_203121.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 1 273.204 20.0 NT2 2 273.204 20.0 NT3 1 273.204 20.0 NT4 2 273.204 20.0 AT1 1 273.204 20.0 230.404 15.880 0.977074 15.516 64 AT2 2 273.204 20.0 AT3 1 273.204 20.0 232.479 21.996 0.977074 21.492 89 AT4 2 273.204 20.0 AT5 1 273.204 20.0 233.596 24.650 0.977074 24.085 100 AT6 2 273.204 20.0 AT7 1 273.204 20.0 231.349 18.582 0.977074 18.156 75 AT8 2 273.204 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 273.204 20.0 NT2 2 273.204 20.0 NT3 1 273.204 20.0 NT4 2 273.204 20.0 AT1 1 273.204 20.0 230.404 15.880 0.977074 15.516 64 AT2 2 273.204 20.0 AT3 1 273.204 20.0 232.479 21.996 0.977074 21.492 89 AT4 2 273.204 20.0 AT5 1 273.204 20.0 233.596 24.650 0.977074 24.085 100 AT6 2 273.204 20.0 AT7 1 273.204 20.0 231.349 18.582 0.977074 18.156 75 AT8 2 273.204 20.0