This paper discusses the parachute subsystem used on an atmospheric entry probe that will descend through the clouds of Jupiter. The entry probe is a part of the Galileo Project to be launched in 1985 aboard the Space Shuttle; the entry probe will encounter the planet in 1988. The parachute subsystem consists of a pilot parachute and a main parachute, and both are of conventional conical ribbon design. Key considerations in the design of the parachutes and a summary of the parachute subsystem test program, which includes two air drop tests and a systems drop test (balloon launched), are presented.


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    Titel :

    Parachute design for Galileo Jupiter entry probe


    Beteiligte:
    Rodier, R. W. (Autor:in) / Thuss, R. C. (Autor:in) / Terhune, J. E. (Autor:in)

    Kongress:

    American Institute of Aeronautics and Astronautics, Aerodynamic Decelerator and Balloon Technology Conference ; 1981 ; San Diego, CA


    Erscheinungsdatum :

    01.10.1981


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Parachute design for Galileo Jupiter entry probe

    RODIER, R. / THUSS, R. / TERHUNE, J. | AIAA | 1981



    Development of a Parachute Mortar Cartridge for the Galileo Jupiter Probe

    Whalley, I. A. / Churchill, J. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2003