Sounding rockets are rocket vehicles designed to carry scientific payloads above the sensible level of the atmosphere. The trajectories of these rockets are very steep, and as a consequence, two important problems arise. These problems are: (1) The dynamic stability of the entire vehicle system as it leaves the atmosphere; (2) The effect of winds on the initial part of the trajectory of such an unguided vehicle. This paper will describe briefly the results of a NASA attempt to cope with these two problems on a particular rocket vehicle.


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    Titel :

    Ascent Problems of Sounding Rockets


    Beteiligte:
    Crabill, N. L. (Autor:in)

    Erscheinungsdatum :

    01.07.1961


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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