Maneuver Plan Plan Date (UTCG): 2011 116 13:56:51 Burn Start (UTCG): 2011 112 18:47:03.6 Pre-burn fuel mass (kg): 115.491 official Maneuver: SK22b Burn Stop (UTCG): 2011 112 18:48:21.2 Post-burn fuel mass (kg): 112.741 official Planned dV (m/s): 5.235 Duration (s): 77.6 Fuel mass used (kg): 2.750 official Average SC Mass (kg): 1134.985 official Notes: SK22b Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK22b_RECON_2011112_184203.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 1 273.400 20.0 NT2 2 273.400 20.0 NT3 1 273.400 20.0 NT4 2 273.400 20.0 AT1 1 273.400 20.0 230.307 15.642 0.982520 15.369 63 AT2 2 273.400 20.0 AT3 1 273.400 20.0 232.480 22.009 0.982520 21.624 89 AT4 2 273.400 20.0 AT5 1 273.400 20.0 233.597 24.664 0.982520 24.233 100 AT6 2 273.400 20.0 AT7 1 273.400 20.0 231.270 18.348 0.982520 18.027 74 AT8 2 273.400 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 273.400 20.0 NT2 2 273.400 20.0 NT3 1 273.400 20.0 NT4 2 273.400 20.0 AT1 1 273.400 20.0 230.307 15.642 0.982520 15.369 63 AT2 2 273.400 20.0 AT3 1 273.400 20.0 232.480 22.009 0.982520 21.624 89 AT4 2 273.400 20.0 AT5 1 273.400 20.0 233.597 24.664 0.982520 24.233 100 AT6 2 273.400 20.0 AT7 1 273.400 20.0 231.270 18.348 0.982520 18.027 74 AT8 2 273.400 20.0