Chinese Space Science and Technology

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ABLATIVE THERMAL PROTECTION STRUCTURE DESIGN OF RETURN MODULE

Chen Qinghua (Beijing Institute of Spacecraft Systems Engineering)   

  • Online:1990-12-25

Abstract: This paper introduces ablative thermal protection structure design of a return module of some satellites. Some concepts, material selection, design appoach, analytical computation and evaluation are given.

Key words: Hot weather construction, Ablative material, Ballistic reentry vehicle, Design