Maneuver Plan

Plan Date (UTCG): 2009 299 16:29:08  Burn Start (UTCG): 2009 296 17:21:45.7  Pre-burn fuel mass (kg):   240.648  official
Maneuver:         SK02b              Burn Stop (UTCG):  2009 296 17:23:21.1  Post-burn fuel mass (kg):  237.218  official
Planned dV (m/s): 5.986              Duration (s):      95.4                 Fuel mass used (kg):         3.430  official
                                                                             Average SC Mass (kg):     1259.805  official
Notes:                        SK02b Calibration
Ephemeris File Name:           
Thrust Vector File Name:      S:\Products\STK Processed Att File\MOC68_SK02b_RECON_2009296_171646.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        271.200           20.0                                                                           
  NT2    2        271.200           20.0                                                                           
  NT3    1        271.200           20.0                                                                           
  NT4    2        271.200           20.0                                                                           
  AT1    1        271.200           20.0        230.668         16.522       0.999631         16.516             67
  AT2    2        271.200           20.0                                                                           
  AT3    1        271.200           20.0        232.379         21.627       0.999631         21.619             88
  AT4    2        271.200           20.0                                                                           
  AT5    1        271.200           20.0        233.581         24.507       0.999631         24.497            100
  AT6    2        271.200           20.0                                                                           
  AT7    1        271.200           20.0        231.571         19.204       0.999631         19.197             78
  AT8    2        271.200           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        271.200           20.0                                                                           
  NT2    2        271.200           20.0                                                                           
  NT3    1        271.200           20.0                                                                           
  NT4    2        271.200           20.0                                                                           
  AT1    1        271.200           20.0        230.668         16.522       0.999631         16.516             67
  AT2    2        271.200           20.0                                                                           
  AT3    1        271.200           20.0        232.379         21.627       0.999631         21.619             88
  AT4    2        271.200           20.0                                                                           
  AT5    1        271.200           20.0        233.581         24.507       0.999631         24.497            100
  AT6    2        271.200           20.0                                                                           
  AT7    1        271.200           20.0        231.571         19.204       0.999631         19.197             78
  AT8    2        271.200           20.0