On-Line Combustion Temperature Measurements of Solid Rocket Propellant by Using Radiation Spectroscopy
YANG Bin1*, GUO Hao-ran1, GUI Xin-yang1, LIU Xin2, WANG Zhi-xin2, CHEN Xiao-long3, LIU Pei-jin2
1. Institute of Particle and Two-Phase Flow Measurement, University of Shanghai for Science and Technology, Shanghai 200093, China
2. Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical University, Xi’an 710072, China
3. Shanghai Space Propulsion Technology Research Institute, Shanghai 201109, China
Abstract：For the high combustion temperature measurement in harsh environment, the radiation spectroscopy method was proposed to realize the online measurement of combustion temperature of solid rocket propellant. The radiation spectrums in the range of 200~1 100 nm of solid rocket propellant flame in high pressure experimental combustor were obtained by fiber-optic spectrometer. Their representative characteristics were summarized, and the corresponding combustion temperature was determined by the Planck radiation law and the spectral fitting method. The paper provides important reference for combustion diagnostics and mechanism of solid rocket propellant.
基金资助: the National Key Research and Development Program of China (2016YFB0600601), the National Natural Science Foundation of China (NSFC) (51327803), Shanghai Academy of Spaceflight Technology (SAST2016099)
通讯作者:
杨 斌
E-mail: yangbin@usst.edu.cn
作者简介: YANG Bin，(1985—)，Ph doctor，lecturer, University of Shanghai for Science and Technology e-mail:
yangbin@usst.edu.cn
引用本文:
杨 斌，郭浩然，桂欣扬，刘 鑫，王志新，陈晓龙，刘佩进. 利用辐射光谱法在线测量固体火箭推进剂燃烧温度[J]. 光谱学与光谱分析, 2018, 38(06): 1958-1962.
YANG Bin, GUO Hao-ran, GUI Xin-yang, LIU Xin, WANG Zhi-xin, CHEN Xiao-long, LIU Pei-jin. On-Line Combustion Temperature Measurements of Solid Rocket Propellant by Using Radiation Spectroscopy. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2018, 38(06): 1958-1962.
[1] Sutton G P. Services Marketing People Technology Strategy, 2010, 8(2): 475.
[2] Chaturvedi S, Dave P N. Arabian Journal of Chemistry, 2015, 106.
[3] Guery J F, Chang I S, Shimada T, et al. Acta Astronautica, 2010, 66(1-2): 201.
[4] Glotov O G, Yagodnikov D A, Vorob’Ev V S, et al. Combustion, Explosion, and Shock Waves, 2007, 43(3): 320.
[5] Law C K. Aiaa Journal, 2012, 50(50): 19.
[6] Hu Z, Liu J, Zhang Z, et al. Chinese Optics Leffers, 2003, 1(7): 395.
[7] Quinn T J. Temperature. New York: Academic Press，1990.
[8] Mu H P, Li Z H, Han Z X, et al. Energy Procedia，2015，66: 133.
[9] Nie B, He X, Zhang C, et al. International Journal of Thermal Sciences, 2014, 78(3): 132.
[10] Fu T, Liu J, Tang J, et al. Infrared Physics & Technology, 2014, 66(9):49.
[11] Jiaxun, Xiaoshu, Zenghao, et al. Frontiers in Energy, 2014, 8(1): 138.
[12] Jiang Z W, Luo Z X, Zhou H C. Fuel, 2009, 88(6): 980.
