| 摘要: |
| 本文论述了固体火箭发动机燃气温度的测量问题,介绍了采用钨铼热电偶测温传感器的测量结果,并介绍使用计算机对燃气温度进行数据采集和处理的研究成果.实验数据与有关计算结果相比较,具有良好的一致性. |
| 关键词: 固体火箭发动机 温度测量 热电偶 |
| DOI： |
| 分类号: |
| 基金项目: |
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| AN INVESTIGATION ON GAS TEMPEATURE MEASUREMENT IN SOLID-PROPELLANT ROCKET ENGINE |
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Li Zhaomin, Wei Yinhua, Geng Qingtao, Wu Lianfu
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Beijing Institute of Technology
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| Abstract: |
| In this paper the gas temperature measurement in solid propellant rocket engine is discussed. By using W-Re thermocouple,and the data acquisition and processing with computer, the gas temperature can be measured. Experimental results agree well with the calculation. |
| Key words: Solid rocket engine Temperature measurement Thermocouple |
