Maneuver Plan Plan Date (UTCG): 2010 236 15:22:15 Burn Start (UTCG): 2010 232 15:14:10.3 Pre-burn fuel mass (kg): 170.527 official Maneuver: SK13b Burn Stop (UTCG): 2010 232 15:15:32.1 Post-burn fuel mass (kg): 167.599 official Planned dV (m/s): 5.312 Duration (s): 81.8 Fuel mass used (kg): 2.928 official Average SC Mass (kg): 1189.935 official Notes: SK13b Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK13b_RECON_2010232_150910.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 1 272.800 20.0 NT2 2 272.800 20.0 NT3 1 272.800 20.0 NT4 2 272.800 20.0 AT1 1 272.800 20.0 230.497 16.107 0.981334 15.807 65 AT2 2 272.800 20.0 AT3 1 272.800 20.0 232.476 21.970 0.981334 21.560 89 AT4 2 272.800 20.0 AT5 1 272.800 20.0 233.593 24.621 0.981334 24.161 100 AT6 2 272.800 20.0 AT7 1 272.800 20.0 231.425 18.805 0.981334 18.454 76 AT8 2 272.800 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 272.800 20.0 NT2 2 272.800 20.0 NT3 1 272.800 20.0 NT4 2 272.800 20.0 AT1 1 272.800 20.0 230.497 16.107 0.981334 15.807 65 AT2 2 272.800 20.0 AT3 1 272.800 20.0 232.476 21.970 0.981334 21.560 89 AT4 2 272.800 20.0 AT5 1 272.800 20.0 233.593 24.621 0.981334 24.161 100 AT6 2 272.800 20.0 AT7 1 272.800 20.0 231.425 18.805 0.981334 18.454 76 AT8 2 272.800 20.0