Maneuver Plan Plan Date (UTCG): 2011 334 14:45:24 Burn Start (UTCG): 2011 331 13:53:55.1 Pre-burn fuel mass (kg): 69.023 official Maneuver: SK30a Burn Stop (UTCG): 2011 331 13:54:48.1 Post-burn fuel mass (kg): 67.171 official Planned dV (m/s): 3.671 Duration (s): 53.0 Fuel mass used (kg): 1.853 official Average SC Mass (kg): 1088.965 official Notes: SK30a Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK30a_RECON_2011331_134855.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 1 272.800 20.0 NT2 2 272.800 20.0 NT3 1 272.800 20.0 NT4 2 272.800 20.0 AT1 1 272.800 20.0 230.202 15.369 0.981563 15.085 62 AT2 2 272.800 20.0 AT3 1 272.800 20.0 232.391 21.728 0.981563 21.327 88 AT4 2 272.800 20.0 AT5 1 272.800 20.0 233.593 24.621 0.981563 24.167 100 AT6 2 272.800 20.0 AT7 1 272.800 20.0 231.105 17.826 0.981563 17.497 72 AT8 2 272.800 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 272.800 20.0 NT2 2 272.800 20.0 NT3 1 272.800 20.0 NT4 2 272.800 20.0 AT1 1 272.800 20.0 230.202 15.369 0.981563 15.085 62 AT2 2 272.800 20.0 AT3 1 272.800 20.0 232.391 21.728 0.981563 21.327 88 AT4 2 272.800 20.0 AT5 1 272.800 20.0 233.593 24.621 0.981563 24.167 100 AT6 2 272.800 20.0 AT7 1 272.800 20.0 231.105 17.826 0.981563 17.497 72 AT8 2 272.800 20.0