Maneuver Plan Plan Date (UTCG): 2014 094 18:46:26 Burn Start (UTCG): 2014 093 17:09:20.0 Pre-burn fuel mass (kg): 41.657 official Maneuver: SK33a Burn Stop (UTCG): 2014 093 17:09:49.0 Post-burn fuel mass (kg): 40.646 official Planned dV (m/s): 2.059 Duration (s): 29.0 Fuel mass used (kg): 1.011 official Average SC Mass (kg): 1062.025 official Notes: SK33a Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK33a_RECON_2014093_170420.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 1 272.900 20.0 NT2 2 272.900 20.0 NT3 1 272.900 20.0 NT4 2 272.900 20.0 AT1 1 272.900 20.0 230.203 15.373 0.983722 15.123 62 AT2 2 272.900 20.0 AT3 1 272.900 20.0 232.307 21.491 0.983722 21.141 87 AT4 2 272.900 20.0 AT5 1 272.900 20.0 233.593 24.628 0.983722 24.227 100 AT6 2 272.900 20.0 AT7 1 272.900 20.0 231.105 17.831 0.983722 17.541 72 AT8 2 272.900 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 272.900 20.0 NT2 2 272.900 20.0 NT3 1 272.900 20.0 NT4 2 272.900 20.0 AT1 1 272.900 20.0 230.203 15.373 0.983722 15.123 62 AT2 2 272.900 20.0 AT3 1 272.900 20.0 232.307 21.491 0.983722 21.141 87 AT4 2 272.900 20.0 AT5 1 272.900 20.0 233.593 24.628 0.983722 24.227 100 AT6 2 272.900 20.0 AT7 1 272.900 20.0 231.105 17.831 0.983722 17.541 72 AT8 2 272.900 20.0