Maneuver Plan Plan Date (UTCG): 2010 316 18:48:01 Burn Start (UTCG): 2010 315 02:05:17.8 Pre-burn fuel mass (kg): 151.671 official Maneuver: SK16b Burn Stop (UTCG): 2010 315 02:06:41.4 Post-burn fuel mass (kg): 148.679 official Planned dV (m/s): 5.501 Duration (s): 83.6 Fuel mass used (kg): 2.992 official Average SC Mass (kg): 1171.045 official Notes: SK16b Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK16b_RECON_2010315_020018.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 1 273.700 20.0 NT2 2 273.700 20.0 NT3 1 273.700 20.0 NT4 2 273.700 20.0 AT1 1 273.700 20.0 230.503 16.149 0.978956 15.810 65 AT2 2 273.700 20.0 AT3 1 273.700 20.0 232.482 22.028 0.978956 21.564 89 AT4 2 273.700 20.0 AT5 1 273.700 20.0 233.599 24.685 0.978956 24.166 100 AT6 2 273.700 20.0 AT7 1 273.700 20.0 231.352 18.609 0.978956 18.217 75 AT8 2 273.700 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 273.700 20.0 NT2 2 273.700 20.0 NT3 1 273.700 20.0 NT4 2 273.700 20.0 AT1 1 273.700 20.0 230.503 16.149 0.978956 15.810 65 AT2 2 273.700 20.0 AT3 1 273.700 20.0 232.482 22.028 0.978956 21.564 89 AT4 2 273.700 20.0 AT5 1 273.700 20.0 233.599 24.685 0.978956 24.166 100 AT6 2 273.700 20.0 AT7 1 273.700 20.0 231.352 18.609 0.978956 18.217 75 AT8 2 273.700 20.0