Maneuver Plan

Plan Date (UTCG): 2014 094 18:46:44  Burn Start (UTCG): 2014 093 20:12:23.0  Pre-burn fuel mass (kg):    40.646  official
Maneuver:         SK33b              Burn Stop (UTCG):  2014 093 20:12:48.4  Post-burn fuel mass (kg):   39.763  official
Planned dV (m/s): 1.803              Duration (s):      25.4                 Fuel mass used (kg):         0.883  official
                                                                             Average SC Mass (kg):     1061.075  official
Notes:                        SK33b Calibration
Ephemeris File Name:           
Thrust Vector File Name:      W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK33b_RECON_2014093_200723.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        272.900           20.0                                                                           
  NT2    2        272.900           20.0                                                                           
  NT3    1        272.900           20.0                                                                           
  NT4    2        272.900           20.0                                                                           
  AT1    1        272.900           20.0        230.098         15.127       0.985681         14.910             61
  AT2    2        272.900           20.0                                                                           
  AT3    1        272.900           20.0        232.307         21.491       0.985681         21.183             87
  AT4    2        272.900           20.0                                                                           
  AT5    1        272.900           20.0        233.593         24.628       0.985681         24.276            100
  AT6    2        272.900           20.0                                                                           
  AT7    1        272.900           20.0        231.105         17.831       0.985681         17.576             72
  AT8    2        272.900           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        272.900           20.0                                                                           
  NT2    2        272.900           20.0                                                                           
  NT3    1        272.900           20.0                                                                           
  NT4    2        272.900           20.0                                                                           
  AT1    1        272.900           20.0        230.098         15.127       0.985681         14.910             61
  AT2    2        272.900           20.0                                                                           
  AT3    1        272.900           20.0        232.307         21.491       0.985681         21.183             87
  AT4    2        272.900           20.0                                                                           
  AT5    1        272.900           20.0        233.593         24.628       0.985681         24.276            100
  AT6    2        272.900           20.0                                                                           
  AT7    1        272.900           20.0        231.105         17.831       0.985681         17.576             72
  AT8    2        272.900           20.0