Maneuver Plan

Plan Date (UTCG): 2009 175 18:30:50  Burn Start (UTCG): 2009 175 10:28:50.2  Pre-burn fuel mass (kg):   478.391  official
Maneuver:         LOI2               Burn Stop (UTCG):  2009 175 10:41:30.2  Post-burn fuel mass (kg):  411.369  official
Planned dV (m/s): 105.466            Duration (s):      760.0                Fuel mass used (kg):        67.022  official
                                                                             Average SC Mass (kg):     1465.750  official
Notes:                        LOI2 Calibration
Ephemeris File Name:           
Thrust Vector File Name:      S:\Products\STK Processed Att File\MOC68_LOI2_RECON_2009175.a

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        268.500           20.0        232.115         93.703       1.021200         95.689            100
  NT2    2        268.500           20.0                                                                           
  NT3    1        268.500           20.0        232.115         93.703       1.021200         95.689            100
  NT4    2        268.500           20.0                                                                           
  AT1    1        268.500           20.0        209.135          1.826       1.021200          1.865              8
  AT2    2        268.500           20.0        200.661          0.000       1.021200          0.000              0
  AT3    1        268.500           20.0        200.661          0.000       1.021200          0.000              0
  AT4    2        268.500           20.0        200.661          0.000       1.021200          0.000              0
  AT5    1        268.500           20.0        211.777          2.579       1.021200          2.633             11
  AT6    2        268.500           20.0        210.926          2.328       1.021200          2.377             10
  AT7    1        268.500           20.0        212.598          2.829       1.021200          2.889             12
  AT8    2        268.500           20.0        211.777          2.579       1.021200          2.633             11

Final Thruster Data:          
                                             Calculated     Calculated         Thrust      Effective           Duty
      Bank    Press (PSI)    Temp (degC)      Isp (sec)     Thrust (N)     Efficiency     Thrust (N)      Cycle (%)
  NT1    1        268.500           20.0        232.115         93.703       1.021200         95.689            100
  NT2    2        268.500           20.0                                                                           
  NT3    1        268.500           20.0        232.115         93.703       1.021200         95.689            100
  NT4    2        268.500           20.0                                                                           
  AT1    1        268.500           20.0        209.135          1.826       1.021200          1.865              8
  AT2    2        268.500           20.0        200.661          0.000       1.021200          0.000              0
  AT3    1        268.500           20.0        200.661          0.000       1.021200          0.000              0
  AT4    2        268.500           20.0        200.661          0.000       1.021200          0.000              0
  AT5    1        268.500           20.0        211.777          2.579       1.021200          2.633             11
  AT6    2        268.500           20.0        210.926          2.328       1.021200          2.377             10
  AT7    1        268.500           20.0        212.598          2.829       1.021200          2.889             12
  AT8    2        268.500           20.0        211.777          2.579       1.021200          2.633             11