[1] 张贵田. 高压补燃液氧/煤油发动机[M]. 北京: 国防工业出版社, 2005.
[2] NICKERSON G R,JOHNSON C W. A soot prediction model for the TDK computer program,AIAA 92-3391[R]. Reston: AIAA, 1992.
[3] VOZOFF M,COULURIS J. Space X products-advancing the use of space, AIAA2008-7836[R]. Reston:AIAA,2008.
[4] LAWVER B R. Test verification of LOX/RP-1 high-pressure fuel/oxidizer rich preburner designs,AIAA82-1153[R]. Reston: AIAA, 1982.
[5] LAWVER B R. Testing of a fuel/oxidizer rich high pressure pre-burner, NASA CR-165609[R]. Madison: Aerojet TechSystems Corporation, 1982.
[6] MERLYN F L, DON C R, et al. Carbon deposition with LOX/RP-1 propellants, AIAA-85-1164[R]. Reston: AIAA, 2008.
[7] HERMANDEZ R, MERCER S D. Carbon deposition characteristics of LO2/HC propellants, AIAA-87-1855[R]. Reston: AIAA, 1987.
[8] FRENKLACH M, RAMACHANDRA M K, MATULA R A. Soot formation in shock-tube oxidation of hydrocarbons[J]. Symposium on combustion, 1985, 20(1):871-878.
[9] FRENKLACH M. Final technical report on kinetics and mechanism of soot formation in hydrocarbon combustion, NAG 3-668[R]. Washington: NASA, 1990.
[10] BOCKHORN H. Soot Formation in combustion, mechanisms and models[M]. Berlin:Springer-Verlag, 1994.
[11] FRENKLACH M. Mechanism of PAH and soot formation and growth[R]. Roam and Haas, Houston, Texas:Conference on Mechanstic Aspects of PAH and Soot Chemistry, 1988.
[12] NICKERSON G R, JOHNSON C W. The chemical kinetics of LOX/hydrocarbon combustion, NAS8-38052[R]. Washington: NASA, 1989.
[13] SONM, Son, KOO J. Conceptual design for a kerosene fuel-rich gas-generator of a turbopump-fed liquid rocket engine[J]. Journal of thermal science 2012, 21(5). 428-434.
[14] LEEC J, YU J M, KOO J Y. Prediction of non-equilibrium kinetics of fuel-rich kerosene/LOX combustion in gas generator, AIAA2007-574[R]. Reston:AIAA, 2007.
[15] DAGAUT P. On the kinetics of hydrocarbons oxidation from natural gas to kerosene and diesel fuel[J]. Phys. Chem., 2002, 4(11): 2079-2094.
[16] 张锋, 严宇, 王延涛, 等. 气氧/煤油富燃燃气发生器燃烧试验研究[J]. 推进技术, 2016, 37(10):1916-1921.