Maneuver Plan Plan Date (UTCG): 2010 288 14:41:05 Burn Start (UTCG): 2010 287 17:20:55.8 Pre-burn fuel mass (kg): 160.930 official Maneuver: SK15a Burn Stop (UTCG): 2010 287 17:22:16.0 Post-burn fuel mass (kg): 158.058 official Planned dV (m/s): 5.236 Duration (s): 80.2 Fuel mass used (kg): 2.872 official Average SC Mass (kg): 1180.365 official Notes: SK15a Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK15a_RECON_2010287_171556.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 1 274.000 20.0 NT2 2 274.000 20.0 NT3 1 274.000 20.0 NT4 2 274.000 20.0 AT1 1 274.000 20.0 230.505 16.163 0.978335 15.813 65 AT2 2 274.000 20.0 AT3 1 274.000 20.0 232.484 22.047 0.978335 21.569 89 AT4 2 274.000 20.0 AT5 1 274.000 20.0 233.601 24.707 0.978335 24.171 100 AT6 2 274.000 20.0 AT7 1 274.000 20.0 231.354 18.625 0.978335 18.221 75 AT8 2 274.000 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 274.000 20.0 NT2 2 274.000 20.0 NT3 1 274.000 20.0 NT4 2 274.000 20.0 AT1 1 274.000 20.0 230.505 16.163 0.978335 15.813 65 AT2 2 274.000 20.0 AT3 1 274.000 20.0 232.484 22.047 0.978335 21.569 89 AT4 2 274.000 20.0 AT5 1 274.000 20.0 233.601 24.707 0.978335 24.171 100 AT6 2 274.000 20.0 AT7 1 274.000 20.0 231.354 18.625 0.978335 18.221 75 AT8 2 274.000 20.0