航天推进技术研究院主办
[1]黄子惟,田松岩,商圣飞.基于双光束干涉原理的微小推力测量系统实验研究[J].火箭推进,2014,40(05):80-85.
HUANG Zi-wei,TIAN Song-yan,SHANG Sheng-fei.Experimental investigation on micro-thrust measurement system based on double-beam interference principle[J].Journal of Rocket Propulsion,2014,40(05):80-85.
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HUANG Zi-wei,TIAN Song-yan,SHANG Sheng-fei.Experimental investigation on micro-thrust measurement system based on double-beam interference principle[J].Journal of Rocket Propulsion,2014,40(05):80-85.
基于双光束干涉原理的微小推力测量系统实验研究
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
40
期数:
2014年05期
页码:
80-85
栏目:
测控与试验
出版日期:
2014-10-28
- Title:
- Experimental investigation on micro-thrust measurement system based on double-beam interference principle
- 分类号:
- V433.9-34
- 文献标志码:
- A
- 摘要:
- 微小推力测量技术是微推进器研制的关键技术之一，是微小卫星技术发展的重要支撑。为了发展更高精度的测量系统，基于双光束干涉原理，提出了一种新的高精度光学微小推力测量方法，设计并搭建了一套测量微小推力的实验装置。进行了三次标定和测量实验，探索和总结出微推力测量的经验和方法，并对测量系统进行改进。实验结果表明，该测量系统使用方便，能获取实时推力曲线，最大测量误差1.86%，测量精度已达到现有推力架的测量精度，但没有达到双光束干涉原理的理论精度要求，在未来有较大的提升空间。
- Abstract:
- The micro-thrust measurement technology plays a key role in micro-thruster development, which is the essential technology of micro-satellite. To develop high-precision measurement system, a new high-precision optical micro-thrust measuring method based on the principle of double-beam interference was proposed, and a micro-thrust experimental device was founded as well. Through three different calibration and measurement tests, some experiences and methods of micro-thrust measurement were obtained and some measuring facilities were improved. The experimental result shows that the measurement system can acquire the real-time thrust curve and is convenient for operation. Its maximum measurement error is 1.86%. The mearuring accuracy is up to the precision of existing thrust-frame measuring equipment. However, the measuring precision is still below the theoretic precision of
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备注/Memo
收稿日期：2014-08-13；修回日期：2014-08-29 作者简介：黄子惟（1992—），男，学士，研究领域为飞行器设计
更新日期/Last Update:
1900-01-01