Three durations of flight between different points of rocket trajectories are shown to be useful in approximate computation of apogee; data from number of flights of known apogee are necessary to establish effects of thrust and drag which are ignored in these computations; results obtained from flights of Black Brant II rockets, launched by National Research Council at Churchill Research Range, are presented and discussed.


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    Titel :

    Some results of rocket apogee computation from flight duration


    Weitere Titelangaben:

    Can Aeronautics Space J


    Beteiligte:
    Steele, K.A. (Autor:in)


    Erscheinungsdatum :

    1966


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :