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火星科学实验室进入舱防热材料的发展及相关气动热试验 被引量：6

Thermal Protective Materials Development and Correlative Aeroheating Tests for MSL Entry Capsule
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摘要 简要回顾了人类火星探测并成功着陆火星的历史,对火星的基本情况及进入环境进行了介绍。对火星科学实验室项目情况、飞向火星的过程及进入气动热环境进行了描述。详细介绍了火星科学实验室进入舱防热材料的发展及相关气动热试验。 The brief historical retrospect on exploring Mars and successfully landing on Mars were carried out. The basic status and entry conditions of Mars were introduced. The Mars Science Laboratory （MSL） program, MSL flying to Mars and the aeroheating conditions endured when entering the Mars atmosphere were described. The thermal protective materials development and eorrelative aeroheating tests for MSL entry capsule were introduced in details.
作者 张友华 陈连忠 张嘉祥 陈智铭
机构地区 中国航天空气动力技术研究院
出处 《宇航材料工艺》 CAS CSCD 北大核心 2012年第6期1-11,共11页 Aerospace Materials & Technology
关键词 火星科学实验室 进入舱 防热材料 气动热试验 MSL, Entry capsule, Thermal protective materials, Aeroheating tests
分类号 V476.4 [航空宇航科学与技术—飞行器设计]
  • 相关文献

参考文献52

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二级参考文献4

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共引文献18

同被引文献66

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  • 8Filippis F D, Vecchio A D, Martucci A. 70MW plasma wind tunnel upgrades for ESA AURORA TPS testing[C]. The 4th International Planetary Probe Workshop, Pasadena California, June 27-30, 2006.
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引证文献6

二级引证文献14

宇航材料工艺
2012年 第6期

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