Maneuver Plan Plan Date (UTCG): 2010 342 19:29:36 Burn Start (UTCG): 2010 341 14:11:43.0 Pre-burn fuel mass (kg): 148.458 official Maneuver: SK17a Burn Stop (UTCG): 2010 341 14:12:59.8 Post-burn fuel mass (kg): 145.702 official Planned dV (m/s): 5.074 Duration (s): 76.8 Fuel mass used (kg): 2.756 official Average SC Mass (kg): 1167.950 official Notes: SK17a Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK17a_RECON_2010341_140643.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 1 274.700 20.0 NT2 2 274.700 20.0 NT3 1 274.700 20.0 NT4 2 274.700 20.0 AT1 1 274.700 20.0 230.510 16.196 0.977521 15.832 65 AT2 2 274.700 20.0 AT3 1 274.700 20.0 232.489 22.091 0.977521 21.595 89 AT4 2 274.700 20.0 AT5 1 274.700 20.0 233.606 24.757 0.977521 24.200 100 AT6 2 274.700 20.0 AT7 1 274.700 20.0 231.359 18.663 0.977521 18.243 75 AT8 2 274.700 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 274.700 20.0 NT2 2 274.700 20.0 NT3 1 274.700 20.0 NT4 2 274.700 20.0 AT1 1 274.700 20.0 230.510 16.196 0.977521 15.832 65 AT2 2 274.700 20.0 AT3 1 274.700 20.0 232.489 22.091 0.977521 21.595 89 AT4 2 274.700 20.0 AT5 1 274.700 20.0 233.606 24.757 0.977521 24.200 100 AT6 2 274.700 20.0 AT7 1 274.700 20.0 231.359 18.663 0.977521 18.243 75 AT8 2 274.700 20.0