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Knowledge Management System of Institue of Mechanics, CAS
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Source Publication：AEROSPACE SCIENCE AND TECHNOLOGY
Funding Organization：National Natural Science Foundation of China(91530112)
Funding Organization：Youth Innovation Foundation of State Key Laboratory of High Temperature Gas Dynamics(LHD2016QN02)
Document Type：期刊论文
Author：李森
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The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 70, 页码: 636-643
Authors:
Li HX(李慧鑫)
;
Ye L(叶亮)
;
Wei XL(魏小林)
;
Li T(李腾)
;
Li S(李森)
;
Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date：2017/12/18
H2o2/kerosene Bipropellant
Coaxial-swirl Injector
Geometric Constant
Performance
