Maneuver Plan

Plan Date (UTCG): 2011 033 17:11:59  Burn Start (UTCG): 2011 031 23:26:40.3  Pre-burn fuel mass (kg):   133.777  official
Maneuver:         SK19b              Burn Stop (UTCG):  2011 031 23:28:01.5  Post-burn fuel mass (kg):  130.889  official
Planned dV (m/s): 5.387              Duration (s):      81.2                 Fuel mass used (kg):         2.888  official
                                                                             Average SC Mass (kg):     1153.205  official
Notes:                        SK19b CALIBRATION
Ephemeris File Name:           
Thrust Vector File Name:      W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK19b_RECON_2011031_232140.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        272.555           20.0                                                                           
  NT2    2        272.555           20.0                                                                           
  NT3    1        272.555           20.0                                                                           
  NT4    2        272.555           20.0                                                                           
  AT1    1        272.555           20.0        230.400         15.850       0.978192         15.504             64
  AT2    2        272.555           20.0                                                                           
  AT3    1        272.555           20.0        232.474         21.955       0.978192         21.476             89
  AT4    2        272.555           20.0                                                                           
  AT5    1        272.555           20.0        233.591         24.604       0.978192         24.067            100
  AT6    2        272.555           20.0                                                                           
  AT7    1        272.555           20.0        231.344         18.547       0.978192         18.143             75
  AT8    2        272.555           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        272.555           20.0                                                                           
  NT2    2        272.555           20.0                                                                           
  NT3    1        272.555           20.0                                                                           
  NT4    2        272.555           20.0                                                                           
  AT1    1        272.555           20.0        230.400         15.850       0.978192         15.504             64
  AT2    2        272.555           20.0                                                                           
  AT3    1        272.555           20.0        232.474         21.955       0.978192         21.476             89
  AT4    2        272.555           20.0                                                                           
  AT5    1        272.555           20.0        233.591         24.604       0.978192         24.067            100
  AT6    2        272.555           20.0                                                                           
  AT7    1        272.555           20.0        231.344         18.547       0.978192         18.143             75
  AT8    2        272.555           20.0