ROCKET ENGINE TYPES
A  B  C  D  E  F  G  H  I  J  K  L  M  N  O  P  Q  R  S  T  U  V  W  X  Y  Z

                  
  • HOME
  • ABOUT
  • CATEGORIES
  • SITE MAP
  • COPYRIGHT
  • ADVERTISE
  • CONTACT


  • entire Web this site



    Fastrac engine

    Fastrac engine testing
    Fastrac engine hot-fire test at Marshall Space Flight Center (NASA/MSFC)
    A low-cost rocket engine, with a thrust of 270,000 newtons, propelled by liquid oxygen and RP-1, that was being developed at the Marshall Space Flight Center as the propulsion unit for the X-34 reusable rocket plane. With the cancellation of the X-34 project in 2001, work on the Fastrac engine also came to a halt. At the time, Fastrac was only the second of about 30 new rocket engines built over the past quarter of a century, to originate in the United States. Fastrac was less expensive than similar engines because of an innovative design approach that used commercial, off-the-shelf parts and fewer of them. Some of its characteristics, including its range of thrust and specific impulse, are shared with the Merlin 1 engine used on SpaceX's Falcon 1.


    Related categories

       • ROCKET ENGINE TYPES
       • ROCKETRY TERMINOLOGY



    Also on this site:

    Encyclopedia of Alternative Energy & Sustainable Living
    Encyclopedia of History
    Transport Concepts & Designs (partner site)



    BACK TO TOP