Three durations of flight between different points of rocket trajectories are shown to be useful in the approximate computation of apogee. Data from a number of flights of known apogee are necessary to establish the effects of thrust and drag which are ignored in these computations. The results obtained from a number of Black Brant II flights are presented and discussed. (Author)


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    Titel :

    Some Results of Rocket Apogee Computation from Flight Duration


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

    Erscheinungsdatum :

    1965


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Some results of rocket apogee computation from flight duration

    Steele, K.A. | Engineering Index Backfile | 1966




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