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Motor Data

Propellant Composition

  • Ammonium Perchlorate -- 70%
  • Aluminum                      -- 10%
  • R45M                              -- 20%

Sustainer Performance

  • Calculated ISP                                        -- 241.5 seconds
  • Maximum Expected Operating Pressure -- 944 psi
  • Burn Time                                               -- 7.0 seconds
  • Maximum Thrust                                    -- 931.5 pounds
  • Propellant Weight                                   -- 23.71 pounds

 

Booster Performance

  • Calculated ISP                                        -- 239.9 seconds
  • Maximum Expected Operating Pressure -- 877 psi
  • Burn Time                                               -- 6.4 seconds
  • Maximum Thrust                                    -- 3549 pounds
  • Propellant Weight                                   -- 80.24 pounds

 

Flight Profile (From Wallops GEM Software)

Motors and motor data supplied by Loki Research.

 

Click graphs for a larger version.