Maneuver Plan

Plan Date (UTCG): 2011 223 18:35:16  Burn Start (UTCG): 2011 222 15:55:24.5  Pre-burn fuel mass (kg):    90.629  official
Maneuver:         SK26b              Burn Stop (UTCG):  2011 222 15:57:41.9  Post-burn fuel mass (kg):   85.794  official
Planned dV (m/s): 9.449              Duration (s):      137.4                Fuel mass used (kg):         4.835  official
                                                                             Average SC Mass (kg):     1109.080  official
Notes:                        SK26b Calibration - Low Periapsis Cycle
Ephemeris File Name:           
Thrust Vector File Name:      W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK26b_RECON_2011222_155024.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        272.000           20.0                                                                           
  NT2    2        272.000           20.0                                                                           
  NT3    1        272.000           20.0                                                                           
  NT4    2        272.000           20.0                                                                           
  AT1    1        272.000           20.0        230.196         15.333       0.985796         15.115             62
  AT2    2        272.000           20.0                                                                           
  AT3    1        272.000           20.0        232.470         21.919       0.985796         21.608             89
  AT4    2        272.000           20.0                                                                           
  AT5    1        272.000           20.0        233.587         24.564       0.985796         24.215            100
  AT6    2        272.000           20.0                                                                           
  AT7    1        272.000           20.0        231.260         18.273       0.985796         18.014             74
  AT8    2        272.000           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        272.000           20.0                                                                           
  NT2    2        272.000           20.0                                                                           
  NT3    1        272.000           20.0                                                                           
  NT4    2        272.000           20.0                                                                           
  AT1    1        272.000           20.0        230.196         15.333       0.985796         15.115             62
  AT2    2        272.000           20.0                                                                           
  AT3    1        272.000           20.0        232.470         21.919       0.985796         21.608             89
  AT4    2        272.000           20.0                                                                           
  AT5    1        272.000           20.0        233.587         24.564       0.985796         24.215            100
  AT6    2        272.000           20.0                                                                           
  AT7    1        272.000           20.0        231.260         18.273       0.985796         18.014             74
  AT8    2        272.000           20.0