Maneuver Plan Plan Date (UTCG): 2015 126 15:05:58 Burn Start (UTCG): 2015 124 15:19:14.2 Pre-burn fuel mass (kg): 36.850 official Maneuver: SK34a Burn Stop (UTCG): 2015 124 15:19:49.8 Post-burn fuel mass (kg): 35.615 official Planned dV (m/s): 2.537 Duration (s): 35.6 Fuel mass used (kg): 1.234 official Average SC Mass (kg): 1057.105 official Notes: SK34a Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK34a_RECON_2015124_150000.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 1 274.200 20.0 NT2 2 274.200 20.0 NT3 1 274.200 20.0 NT4 2 274.200 20.0 AT1 1 274.200 20.0 230.107 15.184 0.988315 15.006 61 AT2 2 274.200 20.0 AT3 1 274.200 20.0 232.233 21.328 0.988315 21.079 86 AT4 2 274.200 20.0 AT5 1 274.200 20.0 233.603 24.721 0.988315 24.432 100 AT6 2 274.200 20.0 AT7 1 274.200 20.0 231.033 17.652 0.988315 17.446 71 AT8 2 274.200 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 274.200 20.0 NT2 2 274.200 20.0 NT3 1 274.200 20.0 NT4 2 274.200 20.0 AT1 1 274.200 20.0 230.107 15.184 0.988315 15.006 61 AT2 2 274.200 20.0 AT3 1 274.200 20.0 232.233 21.328 0.988315 21.079 86 AT4 2 274.200 20.0 AT5 1 274.200 20.0 233.603 24.721 0.988315 24.432 100 AT6 2 274.200 20.0 AT7 1 274.200 20.0 231.033 17.652 0.988315 17.446 71 AT8 2 274.200 20.0