Maneuver Plan

Plan Date (UTCG): 2013 123 14:56:12  Burn Start (UTCG): 2013 119 14:10:47.0  Pre-burn fuel mass (kg):    45.264  official
Maneuver:         SK32a              Burn Stop (UTCG):  2013 119 14:11:00.0  Post-burn fuel mass (kg):   44.809  official
Planned dV (m/s): 0.907              Duration (s):      13.0                 Fuel mass used (kg):         0.456  official
                                                                             Average SC Mass (kg):     1065.905  official
Notes:                        SK32a Calibration
Ephemeris File Name:           
Thrust Vector File Name:      W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK32a_RECON_2013119_140547.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        274.800           20.0                                                                           
  NT2    2        274.800           20.0                                                                           
  NT3    1        274.800           20.0                                                                           
  NT4    2        274.800           20.0                                                                           
  AT1    1        274.800           20.0        230.216         15.458       0.965354         14.922             62
  AT2    2        274.800           20.0                                                                           
  AT3    1        274.800           20.0        232.321         21.609       0.965354         20.861             87
  AT4    2        274.800           20.0                                                                           
  AT5    1        274.800           20.0        233.607         24.764       0.965354         23.906            100
  AT6    2        274.800           20.0                                                                           
  AT7    1        274.800           20.0        231.119         17.929       0.965354         17.308             72
  AT8    2        274.800           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        274.800           20.0                                                                           
  NT2    2        274.800           20.0                                                                           
  NT3    1        274.800           20.0                                                                           
  NT4    2        274.800           20.0                                                                           
  AT1    1        274.800           20.0        230.216         15.458       0.965354         14.922             62
  AT2    2        274.800           20.0                                                                           
  AT3    1        274.800           20.0        232.321         21.609       0.965354         20.861             87
  AT4    2        274.800           20.0                                                                           
  AT5    1        274.800           20.0        233.607         24.764       0.965354         23.906            100
  AT6    2        274.800           20.0                                                                           
  AT7    1        274.800           20.0        231.119         17.929       0.965354         17.308             72
  AT8    2        274.800           20.0