A five-stage solid-fuel sounding-rocket system which can boost a payload of 25 pounds to an altitude of 525 nautical miles and that of 100 pounds to 300 nautical miles is described. Data obtained from a typical flight test of the system are discussed.


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    Titel :

    Five-Stage Solid-Fuel Sounding-Rocket System


    Beteiligte:
    A. G. Swanson (Autor:in)

    Erscheinungsdatum :

    1959


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    SHAVER, R. D. | AIAA | 1967