Maneuver Plan

Plan Date (UTCG): 2011 143 14:13:09  Burn Start (UTCG): 2011 140 19:48:53.8  Pre-burn fuel mass (kg):   109.689  official
Maneuver:         SK23b              Burn Stop (UTCG):  2011 140 19:50:12.8  Post-burn fuel mass (kg):  106.894  official
Planned dV (m/s): 5.360              Duration (s):      79.0                 Fuel mass used (kg):         2.795  official
                                                                             Average SC Mass (kg):     1129.160  official
Notes:                        SK23b Calibration
Ephemeris File Name:           
Thrust Vector File Name:      W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK23b_RECON_2011140_194354.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        230.304         15.620       0.984512         15.378             63
  AT2    2        272.900           20.0                                                                           
  AT3    1        272.900           20.0        232.477         21.977       0.984512         21.636             89
  AT4    2        272.900           20.0                                                                           
  AT5    1        272.900           20.0        233.593         24.628       0.984512         24.247            100
  AT6    2        272.900           20.0                                                                           
  AT7    1        272.900           20.0        231.267         18.321       0.984512         18.037             74
  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        230.304         15.620       0.984512         15.378             63
  AT2    2        272.900           20.0                                                                           
  AT3    1        272.900           20.0        232.477         21.977       0.984512         21.636             89
  AT4    2        272.900           20.0                                                                           
  AT5    1        272.900           20.0        233.593         24.628       0.984512         24.247            100
  AT6    2        272.900           20.0                                                                           
  AT7    1        272.900           20.0        231.267         18.321       0.984512         18.037             74
  AT8    2        272.900           20.0