Maneuver Plan Plan Date (UTCG): 2011 172 18:46:34 Burn Start (UTCG): 2011 167 18:21:16.2 Pre-burn fuel mass (kg): 103.997 official Maneuver: SK24b Burn Stop (UTCG): 2011 167 18:22:32.8 Post-burn fuel mass (kg): 101.290 official Planned dV (m/s): 5.203 Duration (s): 76.6 Fuel mass used (kg): 2.707 official Average SC Mass (kg): 1123.515 official Notes: SK24b Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK24b_RECON_2011167_181616.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 1 272.400 20.0 NT2 2 272.400 20.0 NT3 1 272.400 20.0 NT4 2 272.400 20.0 AT1 1 272.400 20.0 230.300 15.597 0.982153 15.319 63 AT2 2 272.400 20.0 AT3 1 272.400 20.0 232.473 21.945 0.982153 21.553 89 AT4 2 272.400 20.0 AT5 1 272.400 20.0 233.590 24.592 0.982153 24.154 100 AT6 2 272.400 20.0 AT7 1 272.400 20.0 231.263 18.294 0.982153 17.968 74 AT8 2 272.400 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 272.400 20.0 NT2 2 272.400 20.0 NT3 1 272.400 20.0 NT4 2 272.400 20.0 AT1 1 272.400 20.0 230.300 15.597 0.982153 15.319 63 AT2 2 272.400 20.0 AT3 1 272.400 20.0 232.473 21.945 0.982153 21.553 89 AT4 2 272.400 20.0 AT5 1 272.400 20.0 233.590 24.592 0.982153 24.154 100 AT6 2 272.400 20.0 AT7 1 272.400 20.0 231.263 18.294 0.982153 17.968 74 AT8 2 272.400 20.0