Paper shows, by selected examples of experimental French and American missiles, that many aerodynamic problems can lead to failure, if overlooked; most of problems are raised by roll stabilization, by decrease of stability at high Mach numbers, by interaction between propulsive jet and external flow, and by recovery of scientific payloads; it is suggested that specially devised low-density wind-tunnel tests can even help in interpreting some scientific experiments.


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    Titel :

    Aerodynamic problems of sounding-rocket vehicles


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Ceresuela, R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :