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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    Title :

    Trajectory of rocket with thrust


    Additional title:

    Jet Propulsion


    Contributors:

    Published in:

    Jet Propulsion ; 28 , n 7


    Publication date :

    1958


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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