Maneuver Plan

Plan Date (UTCG): 2011 061 14:36:34  Burn Start (UTCG): 2011 058 18:08:50.4  Pre-burn fuel mass (kg):   127.892  official
Maneuver:         SK20b              Burn Stop (UTCG):  2011 058 18:10:10.0  Post-burn fuel mass (kg):  125.072  official
Planned dV (m/s): 5.294              Duration (s):      79.6                 Fuel mass used (kg):         2.820  official
                                                                             Average SC Mass (kg):     1147.350  official
Notes:                        SK20b Calibration
Ephemeris File Name:           
Thrust Vector File Name:      W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK20b_RECON_2011058_180350.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        272.300           20.0                                                                           
  NT2    2        272.300           20.0                                                                           
  NT3    1        272.300           20.0                                                                           
  NT4    2        272.300           20.0                                                                           
  AT1    1        272.300           20.0        230.398         15.838       0.979339         15.511             64
  AT2    2        272.300           20.0                                                                           
  AT3    1        272.300           20.0        232.472         21.938       0.979339         21.485             89
  AT4    2        272.300           20.0                                                                           
  AT5    1        272.300           20.0        233.589         24.585       0.979339         24.077            100
  AT6    2        272.300           20.0                                                                           
  AT7    1        272.300           20.0        231.262         18.289       0.979339         17.911             74
  AT8    2        272.300           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        272.300           20.0                                                                           
  NT2    2        272.300           20.0                                                                           
  NT3    1        272.300           20.0                                                                           
  NT4    2        272.300           20.0                                                                           
  AT1    1        272.300           20.0        230.398         15.838       0.979339         15.511             64
  AT2    2        272.300           20.0                                                                           
  AT3    1        272.300           20.0        232.472         21.938       0.979339         21.485             89
  AT4    2        272.300           20.0                                                                           
  AT5    1        272.300           20.0        233.589         24.585       0.979339         24.077            100
  AT6    2        272.300           20.0                                                                           
  AT7    1        272.300           20.0        231.262         18.289       0.979339         17.911             74
  AT8    2        272.300           20.0