A survey of the general problem of aerothermal reentry is made, showing the complexity of the problem for HERMES as well as for future ASTS. The present status of the TPS solution choosen for HERMES is given. Under consideration are ceramic composites or carbon carbon for hot structures, insulation using for hot zones either ceramic composite shingles plus internal multiscreen insulation or ceramic tiles, and for lower temperature zones flexible external insulation. The difference between HERMES and other potential Space Transportation Systems are studied. A comparison is made between HERMES solutions and other possible TPS systems.


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    Titel :

    Passive thermal protection systems for HERMES


    Weitere Titelangaben:

    Passive Waermeschutzsysteme fuer HERMES


    Beteiligte:
    Chaumette, D. (Autor:in)

    Erschienen in:

    SAE-Papers ; Apr ; 1-5


    Erscheinungsdatum :

    1988


    Format / Umfang :

    5 Seiten, 11 Bilder


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Passive Thermal Protection Systems for HERMES

    Chaumette, D. | SAE Technical Papers | 1988


    Hermes thermal protection system overview

    Chaumette, Daniel / Cretenet, Jean-Claude | Elsevier | 1987



    Hermes Thermal Protection System: An Integrated Concept for Design an Advanced Technologies

    Ackermann, J. / Deutschen Gesellschaft fur Luft- und Raumfahrt eV | British Library Conference Proceedings | 1992


    Hermes Thermal Control Design and Architecture

    Moscatelli, Antonio / Ferro, Claudio / Bottacini, Massimiliano | SAE Technical Papers | 1991