The paper presents the ablative thermal protection structure design of a ballistic reentry spacecraft. The concepts, material selection, design approach, analytical computation and evaluation are described. Thermal protection structure, ablative material, ballistic reentry spacecraft and design.


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    Title :

    Ablative Thermal Protection Structure Design of Ballistic Reentry Spacecraft


    Contributors:
    C. Qinghua (author)

    Publication date :

    1992


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English