Barrier of technical problems prevented actual achievement of attractive predicted capabilities of hybrid propulsion; during past year, effective solutions were found for main problems, including low combustion efficiency, low burning rates, and loss of performance during throttling; combustion process in true hybrid rocket; problem of throttling; range of fuels; comparison of performance characteristics of hybrids with liquids and solids; advantages of clustered hybrid engines.


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    Title :

    Hybrid propulsion


    Additional title:

    Space/Aeronautics


    Contributors:

    Published in:

    Publication date :

    1964


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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