Maneuver Plan Plan Date (UTCG): 2010 207 20:07:08 Burn Start (UTCG): 2010 205 18:39:35.3 Pre-burn fuel mass (kg): 176.746 official Maneuver: SK12b Burn Stop (UTCG): 2010 205 18:40:58.9 Post-burn fuel mass (kg): 173.750 official Planned dV (m/s): 5.417 Duration (s): 83.6 Fuel mass used (kg): 2.996 official Average SC Mass (kg): 1196.120 official Notes: SK12b Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK12b_RECON_2010205_183435.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 1 272.200 20.0 NT2 2 272.200 20.0 NT3 1 272.200 20.0 NT4 2 272.200 20.0 AT1 1 272.200 20.0 230.585 16.325 0.983111 16.049 66 AT2 2 272.200 20.0 AT3 1 272.200 20.0 232.471 21.932 0.983111 21.562 89 AT4 2 272.200 20.0 AT5 1 272.200 20.0 233.588 24.578 0.983111 24.163 100 AT6 2 272.200 20.0 AT7 1 272.200 20.0 231.420 18.772 0.983111 18.455 76 AT8 2 272.200 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 272.200 20.0 NT2 2 272.200 20.0 NT3 1 272.200 20.0 NT4 2 272.200 20.0 AT1 1 272.200 20.0 230.585 16.325 0.983111 16.049 66 AT2 2 272.200 20.0 AT3 1 272.200 20.0 232.471 21.932 0.983111 21.562 89 AT4 2 272.200 20.0 AT5 1 272.200 20.0 233.588 24.578 0.983111 24.163 100 AT6 2 272.200 20.0 AT7 1 272.200 20.0 231.420 18.772 0.983111 18.455 76 AT8 2 272.200 20.0