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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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余西龙 [1]
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Indexed By：SCI
Source Publication：AEROSPACE SCIENCE AND TECHNOLOGY
Funding Project：National Natural Science Foundation of China[11802315]
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Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8
Authors:
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Li F(李飞)
;
Yu XL(余西龙)
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Submit date：2020/05/18
Hybrid rocket engine
Paraffin-based fuel
Acrylonitrile-butadiene-styrene
Regression rate
Combustion efficiency
