Maneuver Plan Plan Date (UTCG): 2014 260 18:20:54 Burn Start (UTCG): 2014 258 19:10:01.9 Pre-burn fuel mass (kg): 38.749 official Maneuver: MOI6 Burn Stop (UTCG): 2014 258 19:10:11.1 Post-burn fuel mass (kg): 38.428 official Planned dV (m/s): 0.636 Duration (s): 9.2 Fuel mass used (kg): 0.321 official Average SC Mass (kg): 1059.460 official Notes: MOI6 (Eclipse Phasing Maneuver) Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_MOI6_RECON_2014258_190500.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 1 273.200 20.0 NT2 2 273.200 20.0 NT3 1 273.200 20.0 NT4 2 273.200 20.0 AT1 1 273.200 20.0 230.205 15.387 0.954660 14.689 62 AT2 2 273.200 20.0 AT3 1 273.200 20.0 232.309 21.510 0.954660 20.535 87 AT4 2 273.200 20.0 AT5 1 273.200 20.0 233.596 24.650 0.954660 23.532 100 AT6 2 273.200 20.0 AT7 1 273.200 20.0 231.107 17.847 0.954660 17.038 72 AT8 2 273.200 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 273.200 20.0 NT2 2 273.200 20.0 NT3 1 273.200 20.0 NT4 2 273.200 20.0 AT1 1 273.200 20.0 230.205 15.387 0.954660 14.689 62 AT2 2 273.200 20.0 AT3 1 273.200 20.0 232.309 21.510 0.954660 20.535 87 AT4 2 273.200 20.0 AT5 1 273.200 20.0 233.596 24.650 0.954660 23.532 100 AT6 2 273.200 20.0 AT7 1 273.200 20.0 231.107 17.847 0.954660 17.038 72 AT8 2 273.200 20.0