Maneuver Plan Plan Date (UTCG): 2018 010 15:37:15 Burn Start (UTCG): 2018 009 15:00:01.6 Pre-burn fuel mass (kg): 27.609 official Maneuver: MOI2 Burn Stop (UTCG): 2018 009 15:00:05.6 Post-burn fuel mass (kg): 27.467 official Planned dV (m/s): 0.273 Duration (s): 4.0 Fuel mass used (kg): 0.142 official Average SC Mass (kg): 1048.410 official Notes: MOI2 (EPM 201801) Calibration Report Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_EPM_201801_RECON_2018009_145501.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 1 272.400 20.0 NT2 2 272.400 20.0 NT3 1 272.400 20.0 NT4 2 272.400 20.0 AT1 1 272.400 20.0 230.494 16.089 0.919042 14.786 65 AT2 2 272.400 20.0 AT3 1 272.400 20.0 232.304 21.460 0.919042 19.723 87 AT4 2 272.400 20.0 AT5 1 272.400 20.0 233.590 24.592 0.919042 22.602 100 AT6 2 272.400 20.0 AT7 1 272.400 20.0 231.343 18.539 0.919042 17.038 75 AT8 2 272.400 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 272.400 20.0 NT2 2 272.400 20.0 NT3 1 272.400 20.0 NT4 2 272.400 20.0 AT1 1 272.400 20.0 230.494 16.089 0.919042 14.786 65 AT2 2 272.400 20.0 AT3 1 272.400 20.0 232.304 21.460 0.919042 19.723 87 AT4 2 272.400 20.0 AT5 1 272.400 20.0 233.590 24.592 0.919042 22.602 100 AT6 2 272.400 20.0 AT7 1 272.400 20.0 231.343 18.539 0.919042 17.038 75 AT8 2 272.400 20.0