| 玻璃型二次表面镜的卫星飞行试验 |
| |
| 引用本文： | 钱盛瑜,王少宏.玻璃型二次表面镜的卫星飞行试验[J].中国空间科学技术,1993,13(6):62-65. |
| |
| 作者姓名： | 钱盛瑜 王少宏 |
| |
| 作者单位： | 北京空间飞行器总体设计部
(钱盛瑜)，兰州物理研究所
(王少宏，邱家稳，常天海)，兰州物理研究所(胡炳森) |
| |
| 摘 要： | 文章介绍了兰州物理研究所研制的石英玻璃型二次表面镜（ＯＳＲ）的卫星搭载试验结果，并对ＯＳＲ的长期空间稳定性作了初步预测。试验和计算结果表明，其ＯＳＲ的太阳吸收率的１０年增值△αｓ预计不超过０．０５５，与国外同类产品的空间稳定性水平相当，已能满足卫星应用的要求。
|
| 关 键 词： | 温控涂层 表面 飞行试验 卫星 |
THE SATELLITE FLYING TEST OF SECONDARY SURFACE MIRROR |
| |
| Qian Shengyu.THE SATELLITE FLYING TEST OF SECONDARY SURFACE MIRROR[J].Chinese Space Science and Technology,1993,13(6):62-65. |
| |
| Authors: | Qian Shengyu |
| |
| Institution: | Qian Shengyu (Beijing Institute of Spacecraft Systems Engineering)
Wang Shaohong Qiu Jiawen Chang Tianhai Hu Bingsen (Lanzhou Institute of Physics) |
| |
| Abstract: | In this paper,the satellite test results of the fused silicasecondary surface mirror (OSR) developed by Lanzhou Institute of Physicshave been reported,and the long-term space stability of OSR has beenestimated.the results of the test and the calculation showed that the 10-yearvariation of solar absorptance of OSR is below 0.05,with the same levelas the foreign products.It can meet the demand of satellite application. |
| |
| Keywords: | Thermal control coating Surface Flight test Satellite |
| 本文献已被 CNKI 维普 等数据库收录！ |
