Role of research rocket and types of vehicle for environmental measurement; design of ballistic rockets; main criteria used in choosing design for Black Knight; development of complete system; first stage has liquid propellant rocket motor using HTP and kerosene which have specific impulse at sea level of 240 sec at 500 lb/sq in.; control and guidance system; second stage; instrumentation; ground facilities; rocket firings.


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    Titel :

    Ballistic research rockets with particular reference to Black Knight


    Weitere Titelangaben:

    Roy Aeronautical Soc -- J


    Beteiligte:
    Lyons, D.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1961


    Format / Umfang :

    19 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Impact points of ballistic rockets

    Roberson, R.E. | Engineering Index Backfile | 1957



    Method for calculating impact points of ballistic rockets

    Singer, S.F. / Wentworth, R.C. | Engineering Index Backfile | 1957


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