ZHANG Xu-hu,WANG Xiang,JIA Zhong-hua,et al.Research progress of the material of small thruster for attitude and orbit control[J].Missiles and Space Vehicles,2005(6):32-37.(in Chinese)
[9]
EDWARDS T.Liquid fuels and propellants for aerospace propulsion:1903-2003[J].Journal of Propulsion and Power,2003,19(6):1 089-1 107.
ZHANG Meng-zheng,TAN Yong-hua.Study of working process of liquid rocket engine[J].Journal of Rocket Propulsion,2002,28(3):1-6,10.(in Chinese)
[12]
杨涛,方丁酉.火箭发动机燃烧原理[M].长沙:国防科技大学出版社,2008.
[13]
YANG Tao,FANG Ding-you.Combustion theory of rocket engine[M].Changsha:National University of Defense Technology Press,2008.(in Chinese)
[14]
YANG L,FU Q,QU Y,et al.Spray characteristics of gelled propellants in swirl injectors[J].Fuel,2012,97(7):253-261.
[15]
PANDIT A V,KUMAR A,SRINIVASA R G,et al.Modeling of liquid propellant combustion chamber[J].Chemical Engineering Journal,2012,207-208(10):151-166.
[16]
LI T,NISHIDA K,HIROYASU H.Droplet size distribution and evaporation characteristics of fuel spray by a swirl type atomizer[J].Fuel,2011,90(7):2 367-2 376.
ZHAO Lin,FAN Wei,FAN Zhen-cen,et al.Experimental investigation on spray characteristics from superheated liquid jets under low pressure[J].Journal of Propulsion Technology,2012,33(5):771-778.(in Chinese)
ZHAO Na,YU Yong-gang.Experiment study on spray characteristics of the swirl injector in small scale chamber[J].Journal of Propulsion Technology,2013,34(7):944-949.(in Chinese)
