| 空间可充气气球应用研究 |
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| 引用本文： | 陈萍萍,孙胜利,黄烽.空间可充气气球应用研究[J].航天电子对抗,2006,22(1):36-38. |
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| 作者姓名： | 陈萍萍 孙胜利 黄烽 |
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| 作者单位： | 中国航天科工集团8511研究所,南京,210007 |
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| 摘 要： | 简述了空间可充气结构的国外应用情况及可充气结构的导弹诱饵和气球卫星,介绍了可充气气球的设计特点,包括采用压力刚化铝箔的刚化结构、充气装置和释放装置,分析了太空环境中原子氧和紫外线辐射对可充气刚化气球的影响程度。
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| 关 键 词： | 可充气 气球卫星 压力刚化铝箔 |
| 修稿时间： | 2005年6月6日 |
Research on the application of inflatable balloons in space |
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| Chen Pingping,Sun Shengli,Huang Feng.Research on the application of inflatable balloons in space[J].Aerospace Electronic Warfare,2006,22(1):36-38. |
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| Authors: | Chen Pingping Sun Shengli Huang Feng |
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| Abstract: | Foreign application status of inflatable structur es,inflatable missile decoys and balloon satellites are briefly introduced.The de sign characteristics of the balloon satellite are described,including rigidizabl e structures of the pressure rigidized aluminum foil,inflatable devices and ejec tors.The affections of atomic oxygen(AO) and UV in space are also analyzed. |
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| Keywords: | inflatable balloon satellite pressure rigidized alu minum foil |
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