| “天宫一号”目标飞行器力学试验新技术应用 |
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| 引用本文： | 岳志勇,冯咬齐,韩晓健.“天宫一号”目标飞行器力学试验新技术应用[J].航天器环境工程,2011,28(6):589-592. |
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| 作者姓名： | 岳志勇 冯咬齐 韩晓健 |
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| 作者单位： | 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 |
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| 摘 要： | “天宫一号”目标飞行器在研制阶段进行的力学环境试验包括模态试验、振动试验、噪声试验.文章总结了各项力学试验的技术难点及新技术的应用情况,可供其他航天器力学试验参考.
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| 关 键 词： | 目标飞行器 模态试验 振动试验 噪声试验 |
| 收稿时间： | 2011/10/28 0:00:00 |
| 修稿时间： | 2011/11/10 0:00:00 |
Application of new techniques in dynamics testing of Tiangong-I target spacecraft |
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| Yue Zhiyong,Feng Yaoqi and Han Xiaojian.Application of new techniques in dynamics testing of Tiangong-I target spacecraft[J].Spacecraft Environment Engineering,2011,28(6):589-592. |
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| Authors: | Yue Zhiyong Feng Yaoqi and Han Xiaojian |
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| Institution: | (Science and Technology on Reliability and Environmental Engineering Laboratory, Beijing Institute of Spacecraft Environment Engineering,Beijing 100094,China) |
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| Abstract: | A set of dynamics tests,including modal testing,vibration testing,and acoustics testing,were performed on Tiangong-I target spacecraft.New techniques applied in the tests and the other key issues are reviewed in this paper,to provide some food of thought for dynamics tests of other spacecraft. |
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| Keywords: | target spacecraft modal testing vibration testing acoustics testing |
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