Maneuver Plan

Plan Date (UTCG): 2011 088 17:01:32  Burn Start (UTCG): 2011 085 13:51:35.5  Pre-burn fuel mass (kg):   124.751  official
Maneuver:         SK21a              Burn Stop (UTCG):  2011 085 13:52:54.5  Post-burn fuel mass (kg):  121.942  official
Planned dV (m/s): 5.269              Duration (s):      79.0                 Fuel mass used (kg):         2.809  official
                                                                             Average SC Mass (kg):     1144.215  official
Notes:                        SK21a Calibration
Ephemeris File Name:           
Thrust Vector File Name:      W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK21a_RECON_2011085_134636.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        273.500           20.0                                                                           
  NT2    2        273.500           20.0                                                                           
  NT3    1        273.500           20.0                                                                           
  NT4    2        273.500           20.0                                                                           
  AT1    1        273.500           20.0        230.406         15.894       0.976002         15.512             64
  AT2    2        273.500           20.0                                                                           
  AT3    1        273.500           20.0        232.481         22.015       0.976002         21.487             89
  AT4    2        273.500           20.0                                                                           
  AT5    1        273.500           20.0        233.598         24.671       0.976002         24.079            100
  AT6    2        273.500           20.0                                                                           
  AT7    1        273.500           20.0        231.271         18.353       0.976002         17.913             74
  AT8    2        273.500           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        273.500           20.0                                                                           
  NT2    2        273.500           20.0                                                                           
  NT3    1        273.500           20.0                                                                           
  NT4    2        273.500           20.0                                                                           
  AT1    1        273.500           20.0        230.406         15.894       0.976002         15.512             64
  AT2    2        273.500           20.0                                                                           
  AT3    1        273.500           20.0        232.481         22.015       0.976002         21.487             89
  AT4    2        273.500           20.0                                                                           
  AT5    1        273.500           20.0        233.598         24.671       0.976002         24.079            100
  AT6    2        273.500           20.0                                                                           
  AT7    1        273.500           20.0        231.271         18.353       0.976002         17.913             74
  AT8    2        273.500           20.0