Dornier-System GmbH proposed development of radio-controlled recoverable and reusable sounding rocket, to reduce expense of experiments; requirements of recovery system for ballistic missiles and considerations which led to system using paraglider, having relatively high position of center of gravity; equipment consists of frame with two profiled aluminum rails, accommodating, flush with outer surface, paraglider beams with rolled-up fabric and nose and stern bulkheads; fitted to frame is fuselage shell, cylindrical stern body and nose cone; paraglider is deployed by means of pneumatic system in beam beds; flight tests and flight stability criteria and future projects.


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    Titel :

    New recovery system for sounding rockets


    Weitere Titelangaben:

    Spaceflight


    Beteiligte:
    Pittelkow, W. (Autor:in)

    Erschienen in:

    Spaceflight ; 9 , n 2


    Erscheinungsdatum :

    1967


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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