中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Study on Kerosene Based Fuel with Hydrogen Peroxide for Hypergolic Application

文献类型:会议论文

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作者Cong Y(丛昱) ; Zhang T(张涛) ; Dou HR(窦和瑞) ; Wang XD(王晓东) ; Liang DB(梁东白) ; Lin G(林革) ; Wang SP(王少鹏) ; Wang YF(王衍方) ; Chen W(陈伟)
出版日期2004-07-02
会议名称space propulsion 2004
会议日期2004-7-2
会议地点意大利
页码166/6
其他题名过氧化氢/煤油自燃推进剂研究
通讯作者张涛
中文摘要hypergolicity is a very important characteristic for bipropellants. with hypergolic propellant, the design of engines and the handling of rocket systems are greatly simplified, and the rocket engine can be restarted repeatedly for a great number of times. hydrogen peroxide and kerosene have been proposed as one of the best potential alternatives for replacing the toxic nitrogen tetroxide and unsymmetrical dimethyl hydrazine bipropellants currently in use. in this paper, composite hypergolic bipropellants have been developed by using high concentration hydrogen peroxide as the oxidizer for kerosene based fuels. the ignition-delay properties as well as the storage stability were extensively examined. reliable ignitions and stable combustion performances were exhibited for over 500 times of cold start firing tests. in addition, satisfactory properties close to that of the traditional toxic hypergolic propellants have been observed in a 5 ton grade thruster.
会议主办者欧洲航天局
学科主题物理化学
语种中文
源URL[http://159.226.238.44/handle/321008/111658]  
专题大连化学物理研究所_中国科学院大连化学物理研究所
推荐引用方式
GB/T 7714
Cong Y,Zhang T,Dou HR,et al. Study on Kerosene Based Fuel with Hydrogen Peroxide for Hypergolic Application, 过氧化氢/煤油自燃推进剂研究[C]. 见:space propulsion 2004. 意大利. 2004-7-2.

入库方式: OAI收割

来源:大连化学物理研究所

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