[1] [1] H. F. Nelson. Infrared radiation signature of tactical rocket exhausts [C]. St. Louis, Missouri: AIAA, 1985: AIAA-82-0913

[2] [2] W. C. Rochelle. Review of Thermal Radiation from Liquid and Solid Propellant Rocket Exhausts [R]. Huntsville: Marshall Space Flight Center, 1967

[3] [3] S. T. Surzhikov. Monte-Carlo Simulation of Plumes Spectral Emission [R]. Institute for Problems in Mechanics Russian Academy of Sciences (IPMech RAS), 2006

[4] [4] J. E. Reardon, Y. C. Lee. A Computer Program for Thermal Radiation from Gaseous Rocket Exhuast Plumes (GASRAD) [R]. NASA-CR-161496, 1980

[5] [5] C. B. Ludwig, W. Malkmus, J. Walker. The standardized infrared radiation mode [C]. AIAA, 1981: AIAA-81-1051

[6] [6] L. H. Liu. Backward Monte Carlo method based on radiation distribution factor [J]. AIAA J. Thermophys., 2004, 18(4): 151～153

[7] [7] Ruan Liming, Qi Hong, Wang Shenggang et al.. Numerical simulation of the infrared characteristic of missile exhaust plume [J]. Infrared and Laser Engineering, 2008, 37(6): 959～962

[8] [8] Jin Wei, Ling Yongshun, Lü Xiangyin. Numerical simulation of the infrared radiation of satellite orbit-control thruster plume [J]. Opto-Electronic Engineering, 2010, 37(10): 6～10

[9] [9] Zhang Xiaoying, Zhu Dingqiang, Cai Guobiao. Study the infrared characteristics of the solid rocket plume with DOM method and the influence of altitude [J]. J. Astronautics, 2007, 28(3): 702～706

[10] [10] S. Feng, W. Nie, Q. Xie et al.. Numerical simulation of flow field and radiation of an aluminized solid-opellant rocket multiphase exhaust plume [C]. Miami, FL: AIAA, 2007:AIAA 2007-4415

[11] [11] W. Wang, Z. Wei, Q. Zhang et al.. Study on infrared signature of solid rocket motor afterburning exhaust plume [C]. Nashville, TN: AIAA, 2010:2010-6847

[12] [12] Guo Aiyan, Bai Tingzhu, Hu Haihe et al.. Analysis of ultraviolet radiation characteristics of solid propellant rocket motor exhaust plume [J]. Acta Optica Sinica, 2012, 32(10): 1016002

[13] [13] Dong Shikui, Tan Heping, Yu Qizheng et al.. Infrared radiative spectral band-model parameters for water vapor in the 300~3000 K temperature range [J]. J. Engineering for Thermal Energy and Power, 2001, 16(1): 33～38

[14] [14] Dong Shikui, Yu Qizheng, Tan Heping et al.. Narrow band model parameters of high temperature radiation for carbon dioxide of combustion products [J]. J. Aerospace Power, 2001, 16(4): 355～359

[15] [15] R. Siegel, R. J. Howell. Thermal Radiation Heat Transfer [M]. Washington D C: Hemisphere and McGraw-Hill, 1981

[16] [16] Tan Heping, Xia Xinlin, Liu Linhua. Numerical Simulation of Infrared Radiation Characteristics and Transfer [M]. Harbin: Harbin Institute of Technology Press, 2006

[17] [17] H. J. Ferziger, M. Peric. Computational Methods for Fluid Dynamics [M]. Berlin: Springer, 1996

[18] [18] A. Devir, A. Lessin, M. Lev et al.. Comparison of calculated and measured radiation from a rocket motor plume [C]. Reno, Nevada: AIAA, 2001:2001-0358

[19] [19] JANNAF HANDBOOK. Rocket Exhaust Plume Technology-Chapter 3 Rocket Exhaust Plume Radiation [R]. Chemical Propulsion Information Agency, 1980