Maneuver Plan Plan Date (UTCG): 2011 306 18:43:48 Burn Start (UTCG): 2011 304 17:03:50.0 Pre-burn fuel mass (kg): 77.033 official Maneuver: SK29a Burn Stop (UTCG): 2011 304 17:05:17.8 Post-burn fuel mass (kg): 73.958 official Planned dV (m/s): 6.087 Duration (s): 87.8 Fuel mass used (kg): 3.075 official Average SC Mass (kg): 1096.365 official Notes: SK29a Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK29a_RECON_2011304_165850.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 20.0 230.199 15.351 0.987181 15.154 62 AT2 2 272.400 20.0 AT3 1 272.400 20.0 232.388 21.702 0.987181 21.424 88 AT4 2 272.400 20.0 AT5 1 272.400 20.0 233.590 24.592 0.987181 24.277 100 AT6 2 272.400 20.0 AT7 1 272.400 20.0 231.183 18.050 0.987181 17.819 73 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 20.0 230.199 15.351 0.987181 15.154 62 AT2 2 272.400 20.0 AT3 1 272.400 20.0 232.388 21.702 0.987181 21.424 88 AT4 2 272.400 20.0 AT5 1 272.400 20.0 233.590 24.592 0.987181 24.277 100 AT6 2 272.400 20.0 AT7 1 272.400 20.0 231.183 18.050 0.987181 17.819 73 AT8 2 272.400 20.0