The present invention relates to a collapsible decelerator for aerial bombs launched from a high velocity vehicle and designed to provide a high drag stabilizer capable of withstanding release in air stream velocities moving at 2600 feet per second. The deceleration includes a hollow inflatable star, the outermost points of which have hooded valve openings through which regulated airflow enters and inflates the star to decelerate the munition to which it is attached. (Author)


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    Titel :

    Inflatable Decelerator


    Beteiligte:
    A. T. Zacharin (Autor:in)

    Erscheinungsdatum :

    1981


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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