Trajectory of aerodynamically stable rocket during its thrust phase is obtained; rocket or missile is interpreted as point mass (with variable weight) acted upon by aerodynamic drag, thrust and gravity; method of solution is best suited to those cases wherein tangential acceleration is large, and may be applied to rocket and missile design problems.


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    Titel :

    Trajectory of rocket with thrust


    Weitere Titelangaben:

    Jet Propulsion


    Beteiligte:
    Struble, R.A. (Autor:in) / Stewart, C.E. (Autor:in) / Granton, Jr., J. (Autor:in)

    Erschienen in:

    Jet Propulsion ; 28 , n 7


    Erscheinungsdatum :

    1958


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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