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	Study on Kerosene Based Fuel with Hydrogen Peroxide for Hypergolic Application; 过氧化氢/煤油自燃推进剂研究
	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)
	2004-07-02
会议名称	space propulsion 2004
会议日期	2004-7-2
会议地点	意大利
其他题名	过氧化氢/煤油自燃推进剂研究
页码	166/6
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
内容类型	会议论文
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.

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