[1] [1] F. Neele, R. Schleijpen. UV missile plume signatures[C]. SPIE, 2002, 4718: 369～379

[2] [2] A. Roblin, P. E. Baudoux, P. Chervet. UV missile plume signatures model[C]. SPIE, 2002, 4718: 344～355

[3] [3] J. M. Burt, I. D. Boyd. High-altitude plume simulations for a solid propellant rocket[J]. AIAA, 2007, 45(12): 2872～2883

[4] [4] W. A. Fiveland. Three-dimensional radiative heat-transfer solutions by the discrete-ordinates method[J]. J. Thermophysics, 1998, 2(4): 309～316

[5] [5] G. P. Sutton, O. Biblarz. Rocket Propulsion Elements[M]. Beijing: Science Press, 2003. 54～62

[6] [6] Wu Xiaosong, Chen Jun, Wang Dong et al.. Numerical Simulations of Working Progress of Solid Rocket Engine[M]. Beijing: High Education Press, 2006. 245～252

[7] [7] F. Neele, R. Schleijpen. Electro-optical missile plume detection[C]. SPIE, 2003, 5075: 270～280

[8] [8] J. L. Rapanotti. FLUENT-based modeling of rocket exhaust signatures[C]. SPIE, 2006, 6239:OS1～10

[9] [9] Tan Heping, Xia Xinlin, Liu Linhua et al.. Numerical Computation of Infrared Radiation and Transmission[M]. Harbin: Harbin Institute of Technology Press, 2006. 25～27

[10] [10] Yu Plastinin, G. Karabadzhak, B. Khmelinin et al.. Ultraviolet, visible and infrared spectra modeling for solid and liquid-fuel rocket exhausts[J]. AIAA, 2001, 0660: 1～6