Maneuver Plan Plan Date (UTCG): 2013 123 14:56:58 Burn Start (UTCG): 2013 119 17:10:31.0 Pre-burn fuel mass (kg): 44.809 official Maneuver: SK32b Burn Stop (UTCG): 2013 119 17:10:56.4 Post-burn fuel mass (kg): 43.921 official Planned dV (m/s): 1.792 Duration (s): 25.4 Fuel mass used (kg): 0.888 official Average SC Mass (kg): 1065.235 official Notes: SK32b Calibration Ephemeris File Name: Thrust Vector File Name: W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK32b_RECON_2013119_170531.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 1 274.900 20.0 NT2 2 274.900 20.0 NT3 1 274.900 20.0 NT4 2 274.900 20.0 AT1 1 274.900 20.0 230.112 15.214 0.978309 14.884 61 AT2 2 274.900 20.0 AT3 1 274.900 20.0 232.321 21.616 0.978309 21.147 87 AT4 2 274.900 20.0 AT5 1 274.900 20.0 233.608 24.771 0.978309 24.234 100 AT6 2 274.900 20.0 AT7 1 274.900 20.0 231.120 17.934 0.978309 17.545 72 AT8 2 274.900 20.0 Final Thruster Data: Calculated Calculated Thrust Effective Duty Bank Press (PSI) Temp (degC) Isp (sec) Thrust (N) Efficiency Thrust (N) Cycle (%) NT1 1 274.900 20.0 NT2 2 274.900 20.0 NT3 1 274.900 20.0 NT4 2 274.900 20.0 AT1 1 274.900 20.0 230.112 15.214 0.978309 14.884 61 AT2 2 274.900 20.0 AT3 1 274.900 20.0 232.321 21.616 0.978309 21.147 87 AT4 2 274.900 20.0 AT5 1 274.900 20.0 233.608 24.771 0.978309 24.234 100 AT6 2 274.900 20.0 AT7 1 274.900 20.0 231.120 17.934 0.978309 17.545 72 AT8 2 274.900 20.0