Maneuver Plan Plan Date (UTCG): 2015 252 13:05:21 Burn Start (UTCG): 2015 247 17:00:01.9 Pre-burn fuel mass (kg): 33.252 official Maneuver: MOI8 Burn Stop (UTCG): 2015 247 17:00:07.7 Post-burn fuel mass (kg): 33.047 official Planned dV (m/s): 0.403 Duration (s): 5.8 Fuel mass used (kg): 0.205 official Average SC Mass (kg): 1054.020 official Notes: MOI8 (EPM 201509) Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_EPM_201509_RECON_2015247_165502.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 1 273.100 20.0 NT2 2 273.100 20.0 NT3 1 273.100 20.0 NT4 2 273.100 20.0 AT1 1 273.100 20.0 230.404 15.875 0.942925 14.969 64 AT2 2 273.100 20.0 AT3 1 273.100 20.0 232.309 21.504 0.942925 20.276 87 AT4 2 273.100 20.0 AT5 1 273.100 20.0 233.595 24.643 0.942925 23.236 100 AT6 2 273.100 20.0 AT7 1 273.100 20.0 231.268 18.332 0.942925 17.285 74 AT8 2 273.100 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 273.100 20.0 NT2 2 273.100 20.0 NT3 1 273.100 20.0 NT4 2 273.100 20.0 AT1 1 273.100 20.0 230.404 15.875 0.942925 14.969 64 AT2 2 273.100 20.0 AT3 1 273.100 20.0 232.309 21.504 0.942925 20.276 87 AT4 2 273.100 20.0 AT5 1 273.100 20.0 233.595 24.643 0.942925 23.236 100 AT6 2 273.100 20.0 AT7 1 273.100 20.0 231.268 18.332 0.942925 17.285 74 AT8 2 273.100 20.0