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红蓝光敏探测器空间环境效应探测数据分析
引用本文:院小雪,易忠,杨东升,刘向鹏,丁义刚,吕红强,臧卫国,刘业楠,于钱,陈金刚.红蓝光敏探测器空间环境效应探测数据分析[J].航天器环境工程,2014,31(5):476-482.
作者姓名:院小雪  易忠  杨东升  刘向鹏  丁义刚  吕红强  臧卫国  刘业楠  于钱  陈金刚
作者单位:1. 北京卫星环境工程研究所, 北京 100094;2. 北京卫星环境工程研究所 可靠性与环境工程技术重点实验室, 北京 100094;3. 深圳航天东方红海特卫星有限公司, 深圳 518064
基金项目:国家国防科技工业局技术基础"十二五"科研项目(编号:科工技[2011]869号)
摘    要:红蓝光敏太阳电池空间环境效应探测器利用镓铟磷和三结砷化镓太阳电池来探测空间污染、原子氧和辐射环境及效应,搭载在中国空间技术研究院自主研制的“新技术验证一号”卫星上。文章通过分析红蓝光敏探测器在轨1年时间的探测数据,得到如下结论:红蓝光敏探测器污染电池板功率下降2.7%,等效污染累积增加量2.23×10^-5 g/cm^2,日均6×10^-8 g/cm^2;原子氧探测器在轨道高度499.226 km运行11个月,原子氧积分通量探测数据为9.7×10^20 AO/cm^2;辐射效应探测器(三结砷化镓太阳电池)在轨1年后累计接受辐射剂量(等效1 MeV电子注量)5.49×10^11 e/cm^2。

关 键 词:空间环境  污染  原子氧  电子辐射  在轨探测
收稿时间:2014/4/29 0:00:00
修稿时间:2014/9/22 0:00:00

The analysis of detected data from the space environment effect detector with red-blue optical sensitivity solar cells
Yuan Xiaoxue,Yi Zhong,Yang Dongsheng,Liu Xiangpeng,Ding Yigang,L&#; Hongqiang,Zang Weiguo,Liu Yenan,Yu Qian,Chen Jin''gang.The analysis of detected data from the space environment effect detector with red-blue optical sensitivity solar cells[J].Spacecraft Environment Engineering,2014,31(5):476-482.
Authors:Yuan Xiaoxue  Yi Zhong  Yang Dongsheng  Liu Xiangpeng  Ding Yigang  L&#; Hongqiang  Zang Weiguo  Liu Yenan  Yu Qian  Chen Jin'gang
Institution:1. Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;2. Science and Technology on Reliability and Environmental Engineering Laboratory, Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China;3. Shenzhen Aerospace Dongfanghong HIT Satellite Co. Ltd, Shenzhen 518064, China
Abstract:The space environment effect detector with red-blue optical sensitivity solar cells, including GaInP2 and GaInP2/GaAs/Ge solar cells, can be used for detecting contamination, atomic oxygen and radiation environment and the related effects. With the detector, a large number of effective detecting data are obtained through XY-1 developed by China Academy of Space Technology. The detected data from the space environment effect detector in one year are analyzed and it is concluded that the power of the contamination detector is declined by 2.7%, the equivalent contamination deposited mass is 2.23×10-5 g/cm2 and the average value is 6×10-8 g/cm2 per day. The atom oxygen flux is 9.7×1020 AO/cm2 in eleven months at the altitude of 499.226 km. The cumulate irradiation dose (equivalent 1 MeV electron fluence) of the radiation effect detector (with three junction GaAs solar cells) for 1 year in orbit is 5.49×1011 e/cm2.
Keywords:space environment  contamination  atomic oxygen  electron radiation  on-orbit detection
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