Maneuver Plan Plan Date (UTCG): 2010 152 18:36:11 Burn Start (UTCG): 2010 150 19:20:56.0 Pre-burn fuel mass (kg): 188.906 official Maneuver: SK10b Burn Stop (UTCG): 2010 150 19:22:16.0 Post-burn fuel mass (kg): 186.044 official Planned dV (m/s): 5.134 Duration (s): 80.0 Fuel mass used (kg): 2.862 official Average SC Mass (kg): 1208.345 official Notes: SK10b Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK10b_RECON_2010150_191500.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 1 271.600 20.0 NT2 2 271.600 20.0 NT3 1 271.600 20.0 NT4 2 271.600 20.0 AT1 1 271.600 20.0 230.581 16.296 0.985426 16.059 66 AT2 2 271.600 20.0 AT3 1 271.600 20.0 232.467 21.894 0.985426 21.575 89 AT4 2 271.600 20.0 AT5 1 271.600 20.0 233.584 24.535 0.985426 24.178 100 AT6 2 271.600 20.0 AT7 1 271.600 20.0 231.416 18.739 0.985426 18.466 76 AT8 2 271.600 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 271.600 20.0 NT2 2 271.600 20.0 NT3 1 271.600 20.0 NT4 2 271.600 20.0 AT1 1 271.600 20.0 230.581 16.296 0.985426 16.059 66 AT2 2 271.600 20.0 AT3 1 271.600 20.0 232.467 21.894 0.985426 21.575 89 AT4 2 271.600 20.0 AT5 1 271.600 20.0 233.584 24.535 0.985426 24.178 100 AT6 2 271.600 20.0 AT7 1 271.600 20.0 231.416 18.739 0.985426 18.466 76 AT8 2 271.600 20.0