Maneuver Plan

Plan Date (UTCG): 2010 207 20:06:27  Burn Start (UTCG): 2010 205 15:41:54.1  Pre-burn fuel mass (kg):   179.828  official
Maneuver:         SK12a              Burn Stop (UTCG):  2010 205 15:43:19.9  Post-burn fuel mass (kg):  176.747  official
Planned dV (m/s): 5.572              Duration (s):      85.8                 Fuel mass used (kg):         3.081  official
                                                                             Average SC Mass (kg):     1199.160  official
Notes:                        SK12a Calibration
Ephemeris File Name:           
Thrust Vector File Name:      W:\LRO\ManeuverTeam\Products\STK Processed Att File\MOC68_SK12a_RECON_2010205_153654.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        230.590         16.358       0.985778         16.125             66
  AT2    2        272.900           20.0                                                                           
  AT3    1        272.900           20.0        232.477         21.977       0.985778         21.664             89
  AT4    2        272.900           20.0                                                                           
  AT5    1        272.900           20.0        233.593         24.628       0.985778         24.278            100
  AT6    2        272.900           20.0                                                                           
  AT7    1        272.900           20.0        231.425         18.810       0.985778         18.543             76
  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        230.590         16.358       0.985778         16.125             66
  AT2    2        272.900           20.0                                                                           
  AT3    1        272.900           20.0        232.477         21.977       0.985778         21.664             89
  AT4    2        272.900           20.0                                                                           
  AT5    1        272.900           20.0        233.593         24.628       0.985778         24.278            100
  AT6    2        272.900           20.0                                                                           
  AT7    1        272.900           20.0        231.425         18.810       0.985778         18.543             76
  AT8    2        272.900           20.0