Maneuver Plan

Plan Date (UTCG): 2011 306 18:44:22  Burn Start (UTCG): 2011 304 19:55:09.0  Pre-burn fuel mass (kg):    73.958  official
Maneuver:         SK29b              Burn Stop (UTCG):  2011 304 19:57:25.6  Post-burn fuel mass (kg):   69.157  official
Planned dV (m/s): 9.510              Duration (s):      136.6                Fuel mass used (kg):         4.801  official
                                                                             Average SC Mass (kg):     1092.430  official
Notes:                        SK29b Calibration
Ephemeris File Name:           
Thrust Vector File Name:      W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK29b_RECON_2011304_195009.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        271.600           20.0                                                                           
  NT2    2        271.600           20.0                                                                           
  NT3    1        271.600           20.0                                                                           
  NT4    2        271.600           20.0                                                                           
  AT1    1        271.600           20.0        230.294         15.561       0.984120         15.314             63
  AT2    2        271.600           20.0                                                                           
  AT3    1        271.600           20.0        232.467         21.894       0.984120         21.546             89
  AT4    2        271.600           20.0                                                                           
  AT5    1        271.600           20.0        233.584         24.535       0.984120         24.146            100
  AT6    2        271.600           20.0                                                                           
  AT7    1        271.600           20.0        231.177         18.008       0.984120         17.722             73
  AT8    2        271.600           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        271.600           20.0                                                                           
  NT2    2        271.600           20.0                                                                           
  NT3    1        271.600           20.0                                                                           
  NT4    2        271.600           20.0                                                                           
  AT1    1        271.600           20.0        230.294         15.561       0.984120         15.314             63
  AT2    2        271.600           20.0                                                                           
  AT3    1        271.600           20.0        232.467         21.894       0.984120         21.546             89
  AT4    2        271.600           20.0                                                                           
  AT5    1        271.600           20.0        233.584         24.535       0.984120         24.146            100
  AT6    2        271.600           20.0                                                                           
  AT7    1        271.600           20.0        231.177         18.008       0.984120         17.722             73
  AT8    2        271.600           20.0