Investigation of Solar Radiation Absorption of Orbit-Control Thruster Plume

Wei JIN; Yong-shun LING; Xiang-yin LV

[1] Li Ziran, Chen Xiaoqian, Zheng Wei, et al. The orbit transfer propulsion systems and the trend of their development [J]. Journal of Rocket Propulsion, 2005, 31(5): 25-31(in Chinese).

[2] Mao Genwang. Present condition and development of advanced propulsion systems on GSO satellites [J]. Journal of Propulsion Technology, 1999, 20(1): 103-107(in Chinese).

[3] Liu Changguo, Zhang Zhongguang, Han Hongyin, et al. Research on the high specific impulse bipropellant liquid apogee engine [J]. Aerospace Shanghai, 2003, (4): 30-33(in Chinese).

[4] Larin M, Lumpkin F, Stuart P. Modeling Unburned Propellant Droplet Distribution and Velocities in Plumes of Small Bipropellant Thrusters [R]. AIAA 2001-2816, 2001.

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

[6] Ludwing C B, Malkus W, Reardon J E, et al. Hand-Book of Infrared Radiation from Combustion [R]. NASA-SP-3080, 1973.

[7] Liu F S, Güilder L, Smallwood G J. Three-dimensional non-grey gas radiative transfer analyses using the statistical narrow-band model [J]. International Journal of Heat Mass Transfer, 1998, 37(9): 759-768.

[8] Saltiel C, Narachi M H N. Parallel processing approach for radiative heat transfer prediction in participating media [J]. Journal of Thermophysics and Heat Transfer, 1993, 7(4): 227-243.

[9] 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(in Chinese).

[10] Howell J R, Perlmuter M. Monte Carlo solution of thermal transfer through radiant media between gray walls [J]. Journal of Heat Transfer, 1997, 8(1):116-122.

[11] Fiveland W A. Three-dimensional radiative heat transfer solutions by the discrete-ordinates approximation [J]. Journal of Thermophysics and Heat Transfer, 1988, 2: 309-316.

[12] Baek S W, Kim M Y. Analysis of radiative heating of a rocket plume base with the finite volume method [J]. International Journal of Heat and Mass Tansfer, 1997, 40(7): 1501-1508.

[13] He Zhihong, Tan Heping, Liu Linhua. Application of finite volume method in calculation of coupled radiation and conduction in cylindrical scattering medium [J]. Journal of Engineering Thermophysics, 2000, 21(3): 338-341(in Chinese).

[14] Wang Fujun. Computational Fluid Dynamics Analysis-Principle and Application of CFD [M]. Beijing: Tsinghua University Press, 2004(in Chinese).

[15] Koo M H, Leap D I. Modeling three-dimensional groundwater flows by the body-fitted coordinate (BFC) method: I. Stationary Boundary problems [J]. Transport in Porous Media, 1998, 30(2): 217-239.

[16] Liu J, Shuang H M, Chen Y S. Prediction of radiative transfer in general body-fitted coordinates [J]. Numerical Heat Tranfer, Part B, 1997, 31: 423-439.