PDF下载分享

[1]胡松启,王鹏飞,刘凯,等.含石蜡燃料初步研究[J].火箭推进,2011,37(06):43-46.
　HU Song-qi,WANG Peng-fei,LIU Kai,et al.Pilot study on solid fuel containing paraffin[J].Journal of Rocket Propulsion,2011,37(06):43-46.

点击复制

含石蜡燃料初步研究

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 37 期数: 2011年06期页码: 43-46 栏目: 燃料与推进剂出版日期: 2011-12-15

Title:: Pilot study on solid fuel containing paraffin

文章编号:: 1672-9374(2011)06-0043-04

作者:: 胡松启; 王鹏飞; 刘凯; 尤琛珣; 官鹏; 西北工业大学燃烧、流动和热结构国家级重点实验室，陕西西安 710072

Author(s):: HU Song-qi; WANG Peng-fei; LIU Kai; YOU Chen-xun; GUAN Peng; National Key Laboratory of Combustion , Flow and Thermo-Structure, Northwestern

关键词:: 预处理石蜡; 固体燃料; 防熔; 退移速率

Keywords:: pre-treatment paraffin; solid fuel; anti-melt; regression rate

分类号:: V51-34

文献标志码:: A

摘要:: 含石蜡燃料具高退移速率特性且成本低，是固液混合发动机理想能源。制取了在气氧矩形燃烧器中燃烧时不发生融化的含石蜡燃料。实验表明：将50％HTPB置换为石蜡，退移速率可提高1.37倍；在燃料中添加金属镁铝合金，可提高燃料密度和退移速率；添加碳黑可提高燃料密度，但退移速率略有下降。

Abstract:: The solid fuel with paraffin is a wonderful hybrid energy source for rocket engine because of its properties of high regression rate and low cost. The solid fuel with paraffin was fabricated by adopting pre-treated paraffin, which was not melted when it combusted in oxygen rectangle-burner. The experiment results show that the regression rate of fuel is increased by a factor of 137% when 50% content of HTPB is replaced with paraffin, the density and regression rate also can be increased consumedly by adding Magnesium-Aluminum alloy to the fuel, and the regression rate is decreased slightly and the density of fuel is increased by adding carbon to the fuel.

参考文献/References:

[1]单建胜, 雷宁. 固液混合发动机的研制及其应用[J]. 固体火箭技术, 1997, 20(3): 13-20.
[2]李宇飞, 何国强, 刘佩进. 固液混合发动机的新宠-石蜡基燃料[J]. 火箭推进, 2005, 31(4): 36-40.
[3]HOPKINS J, SKINNER M, BUCHANAN A, et al. Overview of a 4-inch OD paraffin-based hybrid sounding rocket program, AIAA 2004-3822[R]. USA: AIAA, 2004.
[4]MCCORMICK A, HULTGREN E, LICHTMAN M, et al. Design, optimization, and launch of a 3′ diameter N2O/aluminized paraffin rocket, AIAA 2005-4095[R]. USA: AIAA, 2005.
[5]KARABEYOGLU M A, CANTWELL B J, ALTMAN D．Development and testing of paraffin-based hybrid rocket fuels, AIAA 2001-4503 [R]. USA: AIAA, 2001.
[6]KARABEYOGLU A, ZILLIAC G, CASTELLUCCI P, et al. Development of high-burning-rate hybrid-rocket-fuel flight demonstrations, AIAA2003-5096 [R]. USA: AIAA, 2003.
[7]尤琛珣. 含石蜡燃料热解分析[D]. 西安：西北工业大学, 2008.
[8]官鹏. 含石蜡燃料研制[D]. 西安：西北工业大学, 2010.

备注/Memo

收稿日期：2011-07-04；修回日期：2011-10-19
基金项目：航天支撑基金(NIXA0003)；西北工业大学本科毕业设计（论文）重点扶持基金(W003644)
作者简介：胡松启（1976—），男，副教授，研究领域为固体推进剂及燃烧

更新日期/Last Update: 1900-01-01