Maneuver Plan Plan Date (UTCG): 2015 126 15:06:34 Burn Start (UTCG): 2015 124 18:02:05.2 Pre-burn fuel mass (kg): 35.615 official Maneuver: SK34b Burn Stop (UTCG): 2015 124 18:02:50.2 Post-burn fuel mass (kg): 34.056 official Planned dV (m/s): 3.220 Duration (s): 45.0 Fuel mass used (kg): 1.560 official Average SC Mass (kg): 1055.710 official Notes: SK34b Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK34b_RECON_2015124_180000.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 20.0 230.106 15.175 0.991926 15.052 61 AT2 2 274.000 20.0 AT3 1 274.000 20.0 232.232 21.316 0.991926 21.144 86 AT4 2 274.000 20.0 AT5 1 274.000 20.0 233.601 24.707 0.991926 24.507 100 AT6 2 274.000 20.0 AT7 1 274.000 20.0 231.031 17.642 0.991926 17.500 71 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 20.0 230.106 15.175 0.991926 15.052 61 AT2 2 274.000 20.0 AT3 1 274.000 20.0 232.232 21.316 0.991926 21.144 86 AT4 2 274.000 20.0 AT5 1 274.000 20.0 233.601 24.707 0.991926 24.507 100 AT6 2 274.000 20.0 AT7 1 274.000 20.0 231.031 17.642 0.991926 17.500 71 AT8 2 274.000 20.0