Because the shuttle differs significantly in both geometric and operational characteristics from conventional supersonic aircraft, estimation of sonic boom characteristics required a new technology base. The prediction procedures thus developed are reviewed. Flight measurements obtained for both the ascent and entry phases of the Apollo 15 and 16 and for the ascent phase only of the Apollo 17 missions are presented which verify the techniques established for application to shuttle. Results of extensive analysis of the sonic boom overpressure characteristics completed to date are presented which indicate that this factor of the shuttle's environmental impact is predictable, localized, of short duration and acceptable. Efforts are continuing to define the shuttle sonic boom characteristics to a fine level of detail based on the final system design.


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    Titel :

    Shuttle sonic boom - Technology and predictions


    Beteiligte:
    Holloway, P. F. (Autor:in) / Wilhold, G. A. (Autor:in) / Jones, J. H. (Autor:in) / Garcia, F., Jr. (Autor:in) / Hicks, R. M. (Autor:in)

    Kongress:

    Aero-Acoustics Conference ; 1973 ; Seattle, WA


    Erscheinungsdatum :

    01.10.1973


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Shuttle Sonic Boom - Technology and Predictions

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