A 30-ft-diameter ringslot/solid parachute was designed, developed, and tested at Sandia National Laboratories as the major component of a flight termination system required for a 1900-lb gliding delivery platform. Four full-scale sled tests were performed to validate the design models of the parachute, determine reefing line length, demonstrate structural adequacy of the parachute materials, and demonstrate that performance met the design requirements.


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    Titel :

    Development of a flight termination parachute system for a 1900 lb payload


    Beteiligte:
    D. E. Waye (Autor:in)

    Erscheinungsdatum :

    1997


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    The Development of a Flight Termination Parachute System for a 1900-lb Payload

    Waye, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1997



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