Maneuver Plan Plan Date (UTCG): 2018 186 15:32:58 Burn Start (UTCG): 2018 184 20:38:01.5 Pre-burn fuel mass (kg): 26.456 official Maneuver: MOI3 Burn Stop (UTCG): 2018 184 20:38:12.9 Post-burn fuel mass (kg): 26.063 official Planned dV (m/s): 0.797 Duration (s): 11.4 Fuel mass used (kg): 0.393 official Average SC Mass (kg): 1047.130 official Notes: MOI3 (Eclipse Phasing Maneuver) Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_EPM_201807_RECON_2018184_203300.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 1 271.800 20.0 NT2 2 271.800 20.0 NT3 1 271.800 20.0 NT4 2 271.800 20.0 AT1 1 271.800 20.0 230.090 15.078 0.966684 14.576 61 AT2 2 271.800 20.0 AT3 1 271.800 20.0 232.216 21.180 0.966684 20.475 86 AT4 2 271.800 20.0 AT5 1 271.800 20.0 233.585 24.550 0.966684 23.732 100 AT6 2 271.800 20.0 AT7 1 271.800 20.0 231.015 17.530 0.966684 16.946 71 AT8 2 271.800 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 271.800 20.0 NT2 2 271.800 20.0 NT3 1 271.800 20.0 NT4 2 271.800 20.0 AT1 1 271.800 20.0 230.090 15.078 0.966684 14.576 61 AT2 2 271.800 20.0 AT3 1 271.800 20.0 232.216 21.180 0.966684 20.475 86 AT4 2 271.800 20.0 AT5 1 271.800 20.0 233.585 24.550 0.966684 23.732 100 AT6 2 271.800 20.0 AT7 1 271.800 20.0 231.015 17.530 0.966684 16.946 71 AT8 2 271.800 20.0