Maneuver Plan

Plan Date (UTCG): 2011 088 17:01:59  Burn Start (UTCG): 2011 085 16:49:00.5  Pre-burn fuel mass (kg):   121.942  official
Maneuver:         SK21b              Burn Stop (UTCG):  2011 085 16:50:24.3  Post-burn fuel mass (kg):  118.959  official
Planned dV (m/s): 5.617              Duration (s):      83.8                 Fuel mass used (kg):         2.983  official
                                                                             Average SC Mass (kg):     1141.320  official
Notes:                        SK21b Calibration
Ephemeris File Name:           
Thrust Vector File Name:      W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK21b_RECON_2011085_164401.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        272.900           20.0                                                                           
  NT2    2        272.900           20.0                                                                           
  NT3    1        272.900           20.0                                                                           
  NT4    2        272.900           20.0                                                                           
  AT1    1        272.900           20.0        230.402         15.866       0.977160         15.504             64
  AT2    2        272.900           20.0                                                                           
  AT3    1        272.900           20.0        232.477         21.977       0.977160         21.475             89
  AT4    2        272.900           20.0                                                                           
  AT5    1        272.900           20.0        233.593         24.628       0.977160         24.066            100
  AT6    2        272.900           20.0                                                                           
  AT7    1        272.900           20.0        231.346         18.566       0.977160         18.142             75
  AT8    2        272.900           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        272.900           20.0                                                                           
  NT2    2        272.900           20.0                                                                           
  NT3    1        272.900           20.0                                                                           
  NT4    2        272.900           20.0                                                                           
  AT1    1        272.900           20.0        230.402         15.866       0.977160         15.504             64
  AT2    2        272.900           20.0                                                                           
  AT3    1        272.900           20.0        232.477         21.977       0.977160         21.475             89
  AT4    2        272.900           20.0                                                                           
  AT5    1        272.900           20.0        233.593         24.628       0.977160         24.066            100
  AT6    2        272.900           20.0                                                                           
  AT7    1        272.900           20.0        231.346         18.566       0.977160         18.142             75
  AT8    2        272.900           20.0