Maneuver Plan Plan Date (UTCG): 2011 277 19:05:42 Burn Start (UTCG): 2011 276 20:46:44.6 Pre-burn fuel mass (kg): 80.136 official Maneuver: SK28b Burn Stop (UTCG): 2011 276 20:48:03.6 Post-burn fuel mass (kg): 77.360 official Planned dV (m/s): 5.465 Duration (s): 79.0 Fuel mass used (kg): 2.776 official Average SC Mass (kg): 1099.620 official Notes: SK28b Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK28b_RECON_2011276_204145.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 1 272.600 20.0 NT2 2 272.600 20.0 NT3 1 272.600 20.0 NT4 2 272.600 20.0 AT1 1 272.600 20.0 230.200 15.360 0.984505 15.122 62 AT2 2 272.600 20.0 AT3 1 272.600 20.0 232.474 21.958 0.984505 21.617 89 AT4 2 272.600 20.0 AT5 1 272.600 20.0 233.591 24.607 0.984505 24.225 100 AT6 2 272.600 20.0 AT7 1 272.600 20.0 231.184 18.060 0.984505 17.781 73 AT8 2 272.600 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 272.600 20.0 NT2 2 272.600 20.0 NT3 1 272.600 20.0 NT4 2 272.600 20.0 AT1 1 272.600 20.0 230.200 15.360 0.984505 15.122 62 AT2 2 272.600 20.0 AT3 1 272.600 20.0 232.474 21.958 0.984505 21.617 89 AT4 2 272.600 20.0 AT5 1 272.600 20.0 233.591 24.607 0.984505 24.225 100 AT6 2 272.600 20.0 AT7 1 272.600 20.0 231.184 18.060 0.984505 17.781 73 AT8 2 272.600 20.0