The National Aeronautics and Space Administration needs to be sure the nozzles and heat shields of its new Space Launch System (SLS) rockets will be able to handle the heat generated during liftoff and ascent. Here, Kenyon discusses how engineers at Marshall Space Flight Center are turning to new tools and some Shuffle-era ones to measure the effects of the complicated heat flows that will envelope an SLS on every launch.


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    Titel :

    Modeling heat off rocket engines


    Beteiligte:
    Henry Kenyon (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2015



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch



    Klassifikation :

    Lokalklassifikation TIB:    770/7040
    BKL:    55.88 Luftverkehr, Raumfahrt / 55.88



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    Naraghi, Mohammad / Dunn, Stuart / Coats, Douglas | AIAA | 2005


    Heat pipe cooled rocket engines

    Berkman, D. K. / Toth, J. | NTRS | 1986


    Rocket Engines

    K. Bi-Tien | NTIS | 1976