中国空间科学技术

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弹道式再入航天器的烧蚀防热结构设计

陈清华;   

  1. 北京空间飞行器总体设计部,
  • 发布日期:1990-12-25

ABLATIVE THERMAL PROTECTION STRUCTURE DESIGN OF RETURN MODULE

Chen Qinghua (Beijing Institute of Spacecraft Systems Engineering)   

  • Online:1990-12-25

摘要: 介绍弹道式再入航天器烧蚀防热结构设计,文中说明了方案、材料选择、设计和分析计算。最后评价了这种防热结构。

关键词: 防热结构, 烧蚀材料, 弹道式再入飞行器, 设计

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