Maneuver Plan

Plan Date (UTCG): 2009 177 23:48:18  Burn Start (UTCG): 2009 177 12:24:55.0  Pre-burn fuel mass (kg):   343.990  official
Maneuver:         LOI4               Burn Stop (UTCG):  2009 177 12:35:22.6  Post-burn fuel mass (kg):  288.638  official
Planned dV (m/s): 95.327             Duration (s):      627.6                Fuel mass used (kg):        55.352  official
                                                                             Average SC Mass (kg):     1337.185  official
Notes:                        FDF25 LOI4 Calibration
Ephemeris File Name:           
Thrust Vector File Name:       

Maneuver Configuration:         Bank      1              2              
                                  NT      ON             OFF                 Prop Mode: PressureReg    
                                 ACS      On-Pulsed      On-Pulsed       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        268.560           20.0        232.117         93.722       1.019530         95.552            100
  NT2    2        268.560           20.0                                                                           
  NT3    1        268.560           20.0        232.117         93.722       1.019530         95.552            100
  NT4    2        268.560           20.0                                                                           
  AT1    1        268.560           20.0        207.220          1.324       1.019530          1.350              6
  AT2    2        268.560           20.0        200.661          0.000       1.019530          0.000              0
  AT3    1        268.560           20.0        200.661          0.000       1.019530          0.000              0
  AT4    2        268.560           20.0        200.661          0.000       1.019530          0.000              0
  AT5    1        268.560           20.0        212.599          2.830       1.019530          2.885             12
  AT6    2        268.560           20.0        211.777          2.579       1.019530          2.629             11
  AT7    1        268.560           20.0        212.599          2.830       1.019530          2.885             12
  AT8    2        268.560           20.0        211.777          2.579       1.019530          2.629             11

Final Thruster Data:          
                                             Calculated     Calculated         Thrust      Effective           Duty
      Bank    Press (PSI)    Temp (degC)      Isp (sec)     Thrust (N)     Efficiency     Thrust (N)      Cycle (%)
  NT1    1        268.560           20.0        232.117         93.722       1.019530         95.552            100
  NT2    2        268.560           20.0                                                                           
  NT3    1        268.560           20.0        232.117         93.722       1.019530         95.552            100
  NT4    2        268.560           20.0                                                                           
  AT1    1        268.560           20.0        207.220          1.324       1.019530          1.350              6
  AT2    2        268.560           20.0        200.661          0.000       1.019530          0.000              0
  AT3    1        268.560           20.0        200.661          0.000       1.019530          0.000              0
  AT4    2        268.560           20.0        200.661          0.000       1.019530          0.000              0
  AT5    1        268.560           20.0        212.599          2.830       1.019530          2.885             12
  AT6    2        268.560           20.0        211.777          2.579       1.019530          2.629             11
  AT7    1        268.560           20.0        212.599          2.830       1.019530          2.885             12
  AT8    2        268.560           20.0        211.777          2.579       1.019530          2.629             11