This paper reviews some of the advanced thermal protection systems available for use on future reusable launch vehicles. The systems discussed include advanced carbon-carbon, new high temperature, toughened tiles, and new high temperature ceramic and felt blankets. Based on recent system analyses, a life cycle cost parameter is define and computed for these new thermal protection systems and compared to Shuttle baseline systems, as well as two metallic based concepts.


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    Titel :

    Thermal Protection Systems for Future Reusable Launch Vehicles


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    International Conference on Environmental Systems ; 1995



    Erscheinungsdatum :

    01.07.1995




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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