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
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.
张 杰1，邹彦文1，贺 俊1，杨荣杰2，赵文华3，方仲彦4 . 用光谱诊断技术测定高能单元推进剂的温度分布[J]. 光谱学与光谱分析, 2004, 24(10): 1193-1196.
ZHANG Jie1, ZOU Yan-wen1, HE Jun1, YANG Rong-jie2, ZHAO Wen-hua3, FANG Zhong-yan4 . Temperature Distribution Measurement of High Energetic Monopropellant by Spectroscopic Diagnostic Technology . SPECTROSCOPY AND SPECTRAL ANALYSIS, 2004, 24(10): 1193-1196.
[1] WANG Chang-qi(王长起). Journal of Propellant Technology(推进技术)，1992，13(3)：66. [2] Foltz M F, Coon, C L et al. Propellants, Explosives, Pyrotechnics, 1994，19：19. [3] Wardle B R et al. Proceedings of the 27th ICT Conference on Propellants, Explosives and Pyrotechnics, Karlsruhem 1996, C12-1-11. [4] Huang Yuan he, Zhao Xin qi, Wu Wen hui. Investigation of Structures and Propeertees of HNIW. Proceedings of the Third Beijing International Symposium on Pyrotechnics and Explosives, Beijing, 1995, 11. [5] Foltz M F, Coonm C L et al. Propellants, Explosives, Pyrotechnics, 1994，19: 133. [6] Holtz E et al. Propellants, Explosives, Pyrotechnics, 1994，19: 206. [7] YANG Dong et al. Spectroscopy Letters, 2001, 34(2): 109. [8] YANG Dong, WANG Jun-de, ZHAO Bao-chang，XU He-qian(杨 栋，王俊德，赵宝昌，许和谦). Spectroscopy and Spectral Analysis(光谱学与光谱分析), 2002, 22(2): 307. [9] LIU Da-bin, YANG Dong, JIANG Rong-guang, LI Yan, WANG Jun-de(刘大斌，杨 栋，蒋荣光，李 燕，王俊德). Spectroscopy and Spectral Analysis(光谱学与光谱分析), 2002, 22(4): 670. [10] ZHOU Xin-li, LI Yan, LIU Zu-liang，ZHU Chang-jiang, WANG Jun-de, BAI Chun-xu(周新利，李 燕，刘祖亮，朱长江，王俊德，白春绪). Spectroscopy and Spectral Analysis(光谱学与光谱分析), 2002, 22(5): 764. [11] Zenin A A et al. Combustion, Explosion, and Shock Waves, 1999, 35(5): 532. [12] AN Hong-mei et al(安红梅等). Chinese Journal of Explosives ＆ Propellants(火炸药学报), 2001，24(1): 32.
