航天推进技术研究院主办
[1]凌前程.过氧化氢双组元发动机推力室研究[J].火箭推进,2009,35(04):21-25.
Ling Qiancheng.Investigation on thrust chamber of the hydrogen peroxide bipropellantDIDroDellant engine[J].Journal of Rocket Propulsion,2009,35(04):21-25.
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Ling Qiancheng.Investigation on thrust chamber of the hydrogen peroxide bipropellantDIDroDellant engine[J].Journal of Rocket Propulsion,2009,35(04):21-25.
过氧化氢双组元发动机推力室研究
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
35
期数:
2009年04期
页码:
21-25
栏目:
研究与设计
出版日期:
2009-08-28
- Title:
- Investigation on thrust chamber of the hydrogen peroxide bipropellantDIDroDellant engine
- Keywords:
- hydrogen peroxide; hypogolic fuel; ignition
- 分类号:
- V434
- 文献标志码:
- A
- 摘要:
- 在过氧化氢发动机预先研究项目中，开展了过氧化氢／烃燃料(煤油)推进剂的 自燃点火研究．包括自燃燃料开发、推力室设计及冷、热试考核。设计了25N、30N、50N和 50kN推力量级的推力室。经热试车考核，点火平稳可靠，燃烧稳定，室压粗糙度小于 ±5％，燃烧效率高于92％，设计方案合理。
- Abstract:
- In the research project of hydrogen peroxide engine，the self—ignition researches of hydrogen peroxide and hydrocarbon fuel(kerosene)were performed，including study of hypogolic fuel，design of thrust chamber and hot tests．25N、30N、50N and 50kN thrusters were designed． Successful results of hot——firing tests indicate that self-ignitions are reliable and smooth．The engine has good combustion characteristics and the roughness of chamber pressure is below±5％．the com— bustion efficiency is more than 92％．The design of hydrogen peroxide hypergolic engine was rational
参考文献/References:
[1]Nick Purcell，Amos Diede．Test Results of New Reduced-
Toxicity Hypergols for Use with Hydrogen Peroxide
Oxidizer．The 5th International Hydrogen Peroxider
Propulsion Conference，September 15-19，2002．
[2]Pourpoint T，Rusek，J．Investigation of Homogeneous and
Heterogeneous Catalysis for the Propulsive Decomposition
of Hydrogen Peroxide．The first International Conference
on Green Propellant for Space propulsion。June 20—22，
2001．
[3]Brian M，Mark C．Investigation of Hypergolic Fuels with
Hydrogen Peroxide．AIAA-2001-3837．
[4]Morlan P，Wu P．Catalyst Development for Hydrogen
Peroxide Rocket Engines．AIAA 1999-2740．
[5]Austin B，Heister S．Characterization of Pintle Engine
Performance for Nontoxic Hypergolic Bipropellants．
AIAA一2002--4029．
[61 Long M，Anderson W．Bi-Centiffugal Swirl Injector
Development for Hydrogen Peroxide and Non-Toxic
Hypergolie Miscible Fuels．AIAA-2002-4029．
[7]Sadov V N．HP-Based Green Rocket Propellants．The First
International Conference on Green Propellant for Space
propulsion，June 20—22，2001．
[8]Sadov V N．Self—ignition of Low-toxicity Fuel Diran-A
with Hydrogen Peroxide in Combustion Chamber．The 5th
Intemadonal hydrogrn Peroxider Propulsion Conference，
September 15-19，2002．
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备注/Memo
收稿日期：2009—03—13；修回日期：2009-07-08。 作者简介：凌前程(1976一)，男，工程师，研究领域为液体火箭发动机推力室技术。
更新日期/Last Update:
1900-01-01