|
|
|
|
|
|
Research on Radiation Spectroscopy Thermometry of Plume of Solid Rocket Motor |
GUO Xiao-xu1, PAN Ke-wei2, HOU Long-feng1, YANG Bin1*, PING Li1, XU Qiu-li2, LIU Jin-liang1, WANG Ying1 |
1. School of Energy and Power Engineering; Shanghai Key Laboratory of Multiphase Flow and Heat Transfer in Power Engineering, University of Shanghai for Science and Technology, Shanghai 200093, China
2. Shanghai Space Propulsion Technology Research Institute, Shanghai 201109, China |
|
|
Abstract The plume of solid rocket motor has the characteristics of high temperature, high speed and intense radiation. The temperature of the plume is an essential parameter of condition and performance.The accurate temperature measurement of the plume of a solid rocket motor is important to provide a valuable reference for understanding the internal combustion condition and the overall performance of the motor. With the development of laser and spectroscopy, the laser spectroscopy technology is gradually applied to the measurement of combustion of solid propellant and plume temperature. Radiation spectroscopy thermometry can realize the non-intrusive and on-line measurement of temperature by measuring the radiation spectrum of flame. It has the advantages of wide temperature measuring range, fast response and high reliability. It can be applied to measure the temperature of the plume of the solid rocket motor. In this paper, the thermometry based on radiation spectroscopy was proposed to measure the temperature of the plume of the solid rocket motor. The measurement system of the radiation spectrum of the plume of the solid rocket motor was built using a 350~1 000 nm fiber spectrometer. Moreover, the spectral response coefficient was calibrated with a standard radiation blackbody furnace. The curve of response coefficient with wavelength was obtained to revise the measured radiation spectrums of the plume. Then the measurement system was applied to ground tests of standard Φ118 solid rocket motors, the radiation spectrums of the plume of the solid rocket motor, which with a typical 12% aluminum mass content propellant, were measured. The characteristics of radiation spectrums at different working times were analyzed. Furthermore, the graybody assumption was discussed based on the two-color gray judgment principle. The radiation of plume in a 675~745 nm spectral range can be considered as graybody.The maximum relative deviation of emissivity with wavelength was 4.01%, and the corresponding mean-variance was 1.53%. Therefore, the parameters of temperature and emissivity at the different working times were obtained by spectral fitting based on Planck radiation law. The maximum deviation between the temperature measurement and the theoretical thermodynamic calculation is 5.40%. Besides,the relationship between the measurement results and conditions were discussed, the radiation spectrums of the plume of the solid rocket motors with 12%, 15%, and 19% aluminum mass content propellants were measured, and the characteristics of radiation spectrums with different aluminum mass content were discussed. In addition, the influences of aluminum mass content on radiation spectrums, temperature, and emissivity of the plume were analyzed with the measurement results. This research on radiation spectroscopy thermometry of the plume of the solid rocket motor can provide the tool for performance evaluation and formulation optimization of the solid rocket motor. The influences of aluminum mass content of propellant on radiation spectrums, temperature, and emissivity of the plume can provide the experimental data support for reducing the characteristic signal of the plume of the solid rocket motor.
|
Received: 2019-12-05
Accepted: 2020-05-08
|
|
Corresponding Authors:
YANG Bin
E-mail: yangbin@usst.edu.cn
|
|
[1] Zhao W, Zhu S, Li Y, et al. Journal of Thermophysics and Heat Transfer, 2004, 18(3): 404.
[2] Dennis C, Bojko B. Fuel, 2019, 254: 115646.
[3] Boyarshinov B F, Fedorov S Y. Journal of Applied Mechanics and Technical Physics, 2002, 43(6): 925.
[4] Yang R, Li Y, Zhang J, et al. Combustion and Flame, 2006, 145: 836.
[5] Fu T, Liu J, Duan M, et al. Review of Scientific Instruments, 2014, 85(4): 044901.
[6] Liang M, Sun B, Sun X, et al. Measurement, 2017, 95: 239.
[7] Wang Changhui, Liang Mei, Liang Lei, et al. Spectroscopy and Spectral Analysis, 2018, 38(9): 2860.
[8] Yan W, Zhou H, Lou C, et al. Energy & Fuels, 2013, 27(11): 6754.
[9] Yan W, Li K, Huang X, et al. Energy & Fuels, 2020, 34(1): 907.
[10] Yang Bin, Guo Haoran, Gui Xinyang, et al. Spectroscopy and Spectral Analysis, 2018, 38(6): 1958.
[11] Modest M F. Radiative Heat Transfer. Academic Press, 2003.
[12] National institute of Standards and Technology. NIST Atomic Spectra Database[EB/OL]. http://www.nist.gov/pml/data/asd.cfm.
[13] Sun Yipeng, Lou Chun, Zhou Haichun. Proceedings of the Combustion Institute, 2011, 33: 735. |
[1] |
WANG Wen-song1, PEI Chen-xi2, YANG Bin1*, WANG Zhi-xin2, QIANG Ke-jie2, WANG Ying1. Flame Temperature and Emissivity Distribution Measurement MethodBased on Multispectral Imaging Technology[J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2023, 43(11): 3644-3652. |
[2] |
YU Run-tian1, MA Man-man1, QIN Zhao2*, LIU Guan-nan1, ZHANG Rui1, LIU Dong1*. Study on Diagnostics of Nano Boron-Based Composite Metal Particles in Dispersion Combustion[J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2023, 43(10): 3252-3259. |
[3] |
LIU Qing-song1, DAN You-quan1, YANG Peng2, XU Luo-peng1, YANG Fu-bin1, DENG Nan1. Simulation of Emission Spectrum of Abyssal Methane Based on
HITRAN Database[J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2022, 42(09): 2714-2719. |
[4] |
QI Xin-hua, CHEN Li*, YAN Bo, MU Jin-he, CHEN Shuang, ZHOU Jiang-ning. Velocity Measurement Technology of Supersonic Flow Field Based on Spontaneous Emission Spectrum[J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2021, 41(06): 1745-1750. |
[5] |
WANG Nan1, 2, 3, XUAN Hong-wen3, LI De-hua3, NIE Yu-xin3. Measurement of Speed Distribution of Kerosene Flame by Using Photothermal Deflection Spectroscopy[J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2020, 40(11): 3353-3357. |
[6] |
LIU Yao, TAN Jian-guo*, GAO Zheng-wang. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China[J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2020, 40(04): 1018-1022. |
[7] |
SONG Xu-dong1, GUO Qing-hua2, GONG Yan2*, SU Wei-guang1, BAI Yong-hui1, YU Guang-suo1, 2*. Chemiluminescence Characteristics of Coal-Water Slurry Impinging Flames in Bench-Scale Entrained Flow Gasifier[J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2020, 40(02): 465-471. |
[8] |
ZHU Hui-wen1, HE Lei1, YANG Jia-bao1, GUO Qing-hua1*, GONG Yan1, YU Guang-suo1, 2*. Study on Spectral Characteristics and CH* Distribution Characteristics of Diesel Flames in an Entrained-Flow Gasifier[J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2019, 39(10): 3142-3147. |
[9] |
PING Li1, XIE Jian-wen2, YANG Bin1*, WANG Zhan-ping1, CHEN Yun-chi3, SU Ming-xu1, CAI Xiao-shu1. Research on On-Line Measurements of Radiation Parameters for High-Temperature Particles Based on Radiation Spectroscopy[J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2019, 39(02): 640-645. |
[10] |
YANG Bin1*, GUO Hao-ran1, GUI Xin-yang1, LIU Xin2, WANG Zhi-xin2, CHEN Xiao-long3, LIU Pei-jin2. On-Line Combustion Temperature Measurements of Solid Rocket Propellant by Using Radiation Spectroscopy[J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2018, 38(06): 1958-1962. |
[11] |
YANG Bin1, GUO Hao-ran1, CHEN Xiao-long2, PAN Ke-wei2, GUI Xin-yang1, CAI Xiao-shu1, LIU Pei-jin3. Research on the Influence of Spectral Response on Radiation Spectroscopy Thermometry[J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2018, 38(02): 638-642. |
[12] |
LIU Pei-jin1, WANG Zhi-xin1, YANG Bin2, WEI Xiang-geng1 . Research on Measurement Method of Gas Velocity Combined Absorption Spectroscopy Technique and Cross-Correlation [J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2017, 37(02): 532-536. |
[13] |
GUI Xin-yang, Aymeric Alliot, YANG Bin*, ZHOU Wu, PING Li, CAI Xiao-shu . Research on Radiation Spectrum of Pulverized Coal Combustion Flame [J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2016, 36(11): 3492-3496. |
[14] |
ZHU Guo-ling1,2, KANG Xiao-li2, LUO Jiang-shan2, YI Yong1, YI Zao1, TAN Xiu-lan2, TANG Yong-jian2* . An Analysis of Combustion Emission Spectrum and Combustion Products of KClO4/Zr in the Quartz Tubes [J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2016, 36(09): 2951-2955. |
[15] |
YU Xin1,2, YANG Chao-bo1,2*, PENG Jiang-bo1,2, MA Yu-fei1, 2, 3, LI Xiao-hui1,2, ZHANG Ya-li1,2 . Temperature Measurement of CH4/Air Premix Flat Flame Based on the Absorption Spectroscopy Technology of UV Tunable Laser[J]. SPECTROSCOPY AND SPECTRAL ANALYSIS, 2016, 36(04): 1027-1032. |
|
|
|
|