| 光谱学与光谱分析 |
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| Temperature Distribution Measurement of High Energetic Monopropellant by Spectroscopic Diagnostic Technology |
| ZHANG Jie1, ZOU Yan-wen1, HE Jun1, YANG Rong-jie2, ZHAO Wen-hua3, FANG Zhong-yan4 |
1. Institute of Nuclear Energy Technology, Tsinghua University, Beijing 100084, China
2. School of Materials Science and Engineering, Beijing Institute of Technology, Beijing 100081，China
3. Department of Engineering Mechanicals, Tsinghua University, Beijing 100084, China
4. Department of Precise Instrument and Mechanology，Tsinghua University, Beijing 100084, China |
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Abstract The combustion flame temperature distribution in the axes are measured by relative intensity method of the spectroscopic diagnostic technology for monopropellant hexanitrohexaazaisowurtzitane (HNIW) at 3 MPa and 5 MPa pressure, respectively. The investigation results show that the curves of combustion flame temperature distribution in all combustion course are accurately measured by relative intensity method for monopropellant HNIW. The measured highest combustion flame temperature in the axes are lower than theoretical combustion temperature at the same pressure, and are more close to theoretical combustion temperature along with the rising of the pressure. The experimental results indicate that the combustion flame temperature distribution can be measured by the relative intensity method for high energetic and high burning rate propellant at higher pressure.
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Received: 2004-03-18
Accepted: 2004-06-06
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Corresponding Authors:
ZHANG Jie
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| Cite this article: |
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ZHANG Jie,ZOU Yan-wen,HE Jun, et al. Temperature Distribution Measurement of High Energetic Monopropellant by Spectroscopic Diagnostic Technology [J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2004, 24(10): 1193-1196.
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| URL: |
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http://www.gpxygpfx.com/EN/Y2004/V24/I10/1193 |
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