Maneuver Plan Plan Date (UTCG): 2011 172 18:45:27 Burn Start (UTCG): 2011 167 15:24:12.0 Pre-burn fuel mass (kg): 106.769 official Maneuver: SK24a Burn Stop (UTCG): 2011 167 15:25:30.0 Post-burn fuel mass (kg): 103.997 official Planned dV (m/s): 5.326 Duration (s): 78.0 Fuel mass used (kg): 2.772 official Average SC Mass (kg): 1126.255 official Notes: SK24a Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK24a_RECON_2011167_151910.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 1 273.400 20.0 NT2 2 273.400 20.0 NT3 1 273.400 20.0 NT4 2 273.400 20.0 AT1 1 273.400 20.0 230.307 15.642 0.983919 15.391 63 AT2 2 273.400 20.0 AT3 1 273.400 20.0 232.567 22.251 0.983919 21.894 90 AT4 2 273.400 20.0 AT5 1 273.400 20.0 233.597 24.664 0.983919 24.267 100 AT6 2 273.400 20.0 AT7 1 273.400 20.0 231.270 18.348 0.983919 18.053 74 AT8 2 273.400 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 273.400 20.0 NT2 2 273.400 20.0 NT3 1 273.400 20.0 NT4 2 273.400 20.0 AT1 1 273.400 20.0 230.307 15.642 0.983919 15.391 63 AT2 2 273.400 20.0 AT3 1 273.400 20.0 232.567 22.251 0.983919 21.894 90 AT4 2 273.400 20.0 AT5 1 273.400 20.0 233.597 24.664 0.983919 24.267 100 AT6 2 273.400 20.0 AT7 1 273.400 20.0 231.270 18.348 0.983919 18.053 74 AT8 2 273.400 20.0