Maneuver Plan Plan Date (UTCG): 2010 288 14:41:35 Burn Start (UTCG): 2010 287 20:15:48.8 Pre-burn fuel mass (kg): 158.058 official Maneuver: SK15b Burn Stop (UTCG): 2010 287 20:17:14.0 Post-burn fuel mass (kg): 155.012 official Planned dV (m/s): 5.577 Duration (s): 85.2 Fuel mass used (kg): 3.046 official Average SC Mass (kg): 1177.405 official Notes: SK15b Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK15b_RECON_2010287_201049.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 20.0 230.501 16.135 0.980080 15.814 65 AT2 2 273.400 20.0 AT3 1 273.400 20.0 232.480 22.009 0.980080 21.570 89 AT4 2 273.400 20.0 AT5 1 273.400 20.0 233.597 24.664 0.980080 24.173 100 AT6 2 273.400 20.0 AT7 1 273.400 20.0 231.350 18.593 0.980080 18.222 75 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 20.0 230.501 16.135 0.980080 15.814 65 AT2 2 273.400 20.0 AT3 1 273.400 20.0 232.480 22.009 0.980080 21.570 89 AT4 2 273.400 20.0 AT5 1 273.400 20.0 233.597 24.664 0.980080 24.173 100 AT6 2 273.400 20.0 AT7 1 273.400 20.0 231.350 18.593 0.980080 18.222 75 AT8 2 273.400 20.0