Athena was conceived to reduce cost of ballistic-missile experimentation and employs inexpensive solid-propellant rockets to simulate flight dynamics of intercontinental ballistic missiles; it is four-stage, partially guided vehicle that has been launched from point near Green River, Utah, and impacted at White Sands Missile Range; nominal performance requirements are -- 50-lb payload delivered at 250,000 ft, separation distances (fourth stage from payload) of at least 5000 ft at test altitudes, velocity at test altitudes of 22,000 fps, re-entry angles of 18 to 46°, and payload angle of attack as close to zero as possible.


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    Titel :

    Ballistic-missile research with Athena


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Friedman, R.P. (Autor:in) / Reed, J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Ballistic-missile research with athena

    FRIEDMAN, R. F. / REED, J. | AIAA | 1965


    Ballistic-missile research with athena

    FRIEDMAN, R. / REED, J. | AIAA | 1964


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