Maneuver Plan Plan Date (UTCG): 2011 223 18:34:30 Burn Start (UTCG): 2011 222 13:04:53.5 Pre-burn fuel mass (kg): 95.423 official Maneuver: SK26a Burn Stop (UTCG): 2011 222 13:07:09.7 Post-burn fuel mass (kg): 90.629 official Planned dV (m/s): 9.342 Duration (s): 136.2 Fuel mass used (kg): 4.794 official Average SC Mass (kg): 1113.895 official Notes: SK26a Calibration - Low Periapsis Cycle Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK26a_RECON_2011222_125953.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 1 272.100 20.0 NT2 2 272.100 20.0 NT3 1 272.100 20.0 NT4 2 272.100 20.0 AT1 1 272.100 20.0 230.197 15.337 0.987176 15.141 62 AT2 2 272.100 20.0 AT3 1 272.100 20.0 232.471 21.926 0.987176 21.644 89 AT4 2 272.100 20.0 AT5 1 272.100 20.0 233.588 24.571 0.987176 24.256 100 AT6 2 272.100 20.0 AT7 1 272.100 20.0 231.261 18.279 0.987176 18.044 74 AT8 2 272.100 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 272.100 20.0 NT2 2 272.100 20.0 NT3 1 272.100 20.0 NT4 2 272.100 20.0 AT1 1 272.100 20.0 230.197 15.337 0.987176 15.141 62 AT2 2 272.100 20.0 AT3 1 272.100 20.0 232.471 21.926 0.987176 21.644 89 AT4 2 272.100 20.0 AT5 1 272.100 20.0 233.588 24.571 0.987176 24.256 100 AT6 2 272.100 20.0 AT7 1 272.100 20.0 231.261 18.279 0.987176 18.044 74 AT8 2 272.100 20.0