Maneuver Plan Plan Date (UTCG): 2019 177 20:20:51 Burn Start (UTCG): 2019 175 17:10:01.3 Pre-burn fuel mass (kg): 24.031 official Maneuver: MOI4 Burn Stop (UTCG): 2019 175 17:10:12.1 Post-burn fuel mass (kg): 23.657 official Planned dV (m/s): 0.758 Duration (s): 10.8 Fuel mass used (kg): 0.374 official Average SC Mass (kg): 1044.715 official Notes: EPM 201907 (MOI4) Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_EPM_201907_RECON_2019175_170501.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 1 272.600 20.0 NT2 2 272.600 20.0 NT3 1 272.600 20.0 NT4 2 272.600 20.0 AT1 1 272.600 20.0 230.096 15.113 0.964061 14.570 61 AT2 2 272.600 20.0 AT3 1 272.600 20.0 232.222 21.230 0.964061 20.467 86 AT4 2 272.600 20.0 AT5 1 272.600 20.0 233.591 24.607 0.964061 23.722 100 AT6 2 272.600 20.0 AT7 1 272.600 20.0 231.103 17.816 0.964061 17.175 72 AT8 2 272.600 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 272.600 20.0 NT2 2 272.600 20.0 NT3 1 272.600 20.0 NT4 2 272.600 20.0 AT1 1 272.600 20.0 230.096 15.113 0.964061 14.570 61 AT2 2 272.600 20.0 AT3 1 272.600 20.0 232.222 21.230 0.964061 20.467 86 AT4 2 272.600 20.0 AT5 1 272.600 20.0 233.591 24.607 0.964061 23.722 100 AT6 2 272.600 20.0 AT7 1 272.600 20.0 231.103 17.816 0.964061 17.175 72 AT8 2 272.600 20.0