Ramjet propulsion using solid propellant for post-boost acceleration of missiles exhibits several favorable properties, brought about by heterogeneous combustion. A simplified theory for calculating the performance of possible propellants classified with respect to maximum fuel-specific impulse, is presented. The optimal choice of fuel, from a system standpoint, must consider volume constraints, and defines the requirements for motor geometry. (Author)


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    Titel :

    Propellant Selection for Ramjets with Solid Fuel


    Beteiligte:
    R. H. Schmucker (Autor:in) / H. Lips (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    33 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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