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。
Foreign application status of inflatable structures, inflatable missile decoys and balloon satellites are briefly introduced. The design characteristics of the balloon satellite are described, including rigidizable structures of the pressure rigidized aluminum foil, inflatable devices and ejectors. The affections of atomic oxygen （AO） and UV in space are also analyzed.
出处
《航天电子对抗》
2006年第1期36-38,共3页
Aerospace Electronic Warfare
关键词
可充气
气球卫星
压力刚化铝箔
inflatable
balloon satellite
pressure rigidized aluminum foil
