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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Some results of rocket apogee computation from flight duration


    Additional title:

    Can Aeronautics Space J


    Contributors:


    Publication date :

    1966


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English