Modern achievements and the problems of powerful Liquid Rocket Engines (LRE) for launch system main propulsion units are shown. Results of LRE research and development carried out in Russia are included. LRE's have been used since the beginning of the forties. Many investigations were carried out on the design of high efficiency LRE's and the technology for engine development and production. Recent data and technology have led to the development of LRE's which have parameters that are close to the upper design limits.


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    Title :

    Cryogenic Propellant Rocket Engine Problems


    Contributors:
    A. Roudakov (author)

    Publication date :

    1993


    Size :

    106 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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