Maneuver Plan

Plan Date (UTCG): 2010 047 13:49:05  Burn Start (UTCG): 2010 040 18:18:24.4  Pre-burn fuel mass (kg):   214.717  official
Maneuver:         SK06b              Burn Stop (UTCG):  2010 040 18:19:56.8  Post-burn fuel mass (kg):  211.421  official
Planned dV (m/s): 5.847              Duration (s):      92.4                 Fuel mass used (kg):         3.296  official
                                                                             Average SC Mass (kg):     1233.940  official
Notes:                        SK06b Calibration
Ephemeris File Name:           
Thrust Vector File Name:      S:\Products\STK Processed Att File\MOC68_SK06b_RECON_2010040_181324.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        270.500           20.0                                                                           
  NT2    2        270.500           20.0                                                                           
  NT3    1        270.500           20.0                                                                           
  NT4    2        270.500           20.0                                                                           
  AT1    1        270.500           20.0        230.573         16.244       0.995350         16.168             66
  AT2    2        270.500           20.0                                                                           
  AT3    1        270.500           20.0        232.374         21.582       0.995350         21.482             88
  AT4    2        270.500           20.0                                                                           
  AT5    1        270.500           20.0        233.576         24.456       0.995350         24.343            100
  AT6    2        270.500           20.0                                                                           
  AT7    1        270.500           20.0        231.487         18.922       0.995350         18.834             77
  AT8    2        270.500           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        270.500           20.0                                                                           
  NT2    2        270.500           20.0                                                                           
  NT3    1        270.500           20.0                                                                           
  NT4    2        270.500           20.0                                                                           
  AT1    1        270.500           20.0        230.573         16.244       0.995350         16.168             66
  AT2    2        270.500           20.0                                                                           
  AT3    1        270.500           20.0        232.374         21.582       0.995350         21.482             88
  AT4    2        270.500           20.0                                                                           
  AT5    1        270.500           20.0        233.576         24.456       0.995350         24.343            100
  AT6    2        270.500           20.0                                                                           
  AT7    1        270.500           20.0        231.487         18.922       0.995350         18.834             77
  AT8    2        270.500           20.0