An improved understanding of low gravity subcritical cryogenic fluid behavior is critical for the continued development of space based systems. Although early experimental programs provided some fundamental understanding of zero gravity cryogenic fluid behavior, more extensive flight data are required to design space based cryogenic liquid storage and transfer systems with confidence. As NASA's mission concepts evolve, the demand for optimized in-space cryogenic systems is increasing. Cryogenic Orbital Nitrogen Experiment (CONE) is an attached shuttle payload experiment designed to address major technological issues associated with on-orbit storage and supply of cryogenic liquids. During its 7 day mission, CONE will conduct experiments and technology demonstrations in active and passive pressure control, stratification and mixing, liquid delivery and expulsion efficiency, and pressurant bottle recharge. These experiments, conducted with liquid nitrogen as the test fluid, will substantially extend the existing low gravity fluid data base and will provide future system designers with vital performance data from an orbital environment.


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    Titel :

    Feasibility Study for the Cryogenic Orbital Nitrogen Experiment (CONE)


    Beteiligte:
    R. S. Bell (Autor:in) / M. A. Crouch (Autor:in) / G. J. Hanna (Autor:in) / E. C. Cady (Autor:in) / J. S. Meserole (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    212 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch