The state of the art in passive reusable thermal protection system materials is described. Development of the Space Shuttle Orbiter, which was the first reusable vehicle, is discussed. The thermal protection materials and given concepts and some of the shuttle development and manufacturing problems are described. Evolution of a family of grid and flexible ceramic external insulation materials from the initial shuttle concept in the early 1970's to the present time is described. The important properties and their evolution are documented. Application of these materials to vehicles currently being developed and plans for research to meet the space programs future needs are summarized.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Reusable Thermal Protection System Development: A Prospective


    Beteiligte:
    H. Goldstein (Autor:in)

    Erscheinungsdatum :

    1992


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Reusable Metallic Thermal Protection Systems Development

    Blosser, M. L. et al. | British Library Conference Proceedings | 1998


    Thermal Protection System for Reusable Launch Vehicles

    Pace, Patrick / Maji, Arup | ASCE | 2008


    High heat transfer rate reusable thermal protection system

    HERZBERG JAMES S / BUDICA ROBERT J / CHANDLER FRANK O et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    HIGH HEAT TRANSFER RATE REUSABLE THERMAL PROTECTION SYSTEM

    KHERTSBERG DZHEJMS S / BUDIKA ROBERT DZH / CHANDLER FRENK O et al. | Europäisches Patentamt | 2019

    Freier Zugriff