Maneuver Plan

Plan Date (UTCG): 2011 116 13:56:03  Burn Start (UTCG): 2011 112 15:51:26.6  Pre-burn fuel mass (kg):   118.605  official
Maneuver:         SK22a              Burn Stop (UTCG):  2011 112 15:52:54.4  Post-burn fuel mass (kg):  115.491  official
Planned dV (m/s): 5.935              Duration (s):      87.8                 Fuel mass used (kg):         3.114  official
                                                                             Average SC Mass (kg):     1137.920  official
Notes:                        SK22a Calibration
Ephemeris File Name:           
Thrust Vector File Name:      W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK22a_RECON_2011112_154626.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        273.700           20.0                                                                           
  NT2    2        273.700           20.0                                                                           
  NT3    1        273.700           20.0                                                                           
  NT4    2        273.700           20.0                                                                           
  AT1    1        273.700           20.0        230.310         15.656       0.986238         15.440             63
  AT2    2        273.700           20.0                                                                           
  AT3    1        273.700           20.0        232.482         22.028       0.986238         21.724             89
  AT4    2        273.700           20.0                                                                           
  AT5    1        273.700           20.0        233.599         24.685       0.986238         24.346            100
  AT6    2        273.700           20.0                                                                           
  AT7    1        273.700           20.0        231.272         18.364       0.986238         18.111             74
  AT8    2        273.700           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        273.700           20.0                                                                           
  NT2    2        273.700           20.0                                                                           
  NT3    1        273.700           20.0                                                                           
  NT4    2        273.700           20.0                                                                           
  AT1    1        273.700           20.0        230.310         15.656       0.986238         15.440             63
  AT2    2        273.700           20.0                                                                           
  AT3    1        273.700           20.0        232.482         22.028       0.986238         21.724             89
  AT4    2        273.700           20.0                                                                           
  AT5    1        273.700           20.0        233.599         24.685       0.986238         24.346            100
  AT6    2        273.700           20.0                                                                           
  AT7    1        273.700           20.0        231.272         18.364       0.986238         18.111             74
  AT8    2        273.700           20.0