航天推进技术研究院主办
[1]丰松江,何博,聂万胜.液体火箭凝胶推进剂燃烧特性研究进展[J].火箭推进,2009,35(04):1-7.
Feng Songjiang,He Bo,Nie Wansheng.Progress in combustion characteristic research of liquid rocket gelled propellants[J].Journal of Rocket Propulsion,2009,35(04):1-7.
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Feng Songjiang,He Bo,Nie Wansheng.Progress in combustion characteristic research of liquid rocket gelled propellants[J].Journal of Rocket Propulsion,2009,35(04):1-7.
液体火箭凝胶推进剂燃烧特性研究进展
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
35
期数:
2009年04期
页码:
1-7
栏目:
专论与综述
出版日期:
2009-08-28
- Title:
- Progress in combustion characteristic research of liquid rocket gelled propellants
- Keywords:
- gelled propellants; combustion; research progress
- 分类号:
- V434
- 文献标志码:
- A
- 摘要:
- 液体火箭凝胶推进剂燃烧特性是凝胶推进技术发展的关键问题之一。综述了液 体火箭凝胶推进剂燃烧特性研究状况与进展．详细阐述了凝胶液滴燃烧机理，总结分析了凝 胶推进剂燃烧特性三种试验研究方案和四种理论研究模型的特点，指出了研究凝胶推进剂燃 烧特性的重要性并对进一步的研究工作提出建议。
- Abstract:
- Combustion characteristic of liquid rocket gelled propellants is one of the key prob— lems for development of gelled propulsion technology．Research and development of combustion characteristic of liquid rocket gelled propellants were summarized．The combustion mechanisms of gelled propellants droplets were introduced．The characteristics of three kinds of experimental schemes and four kinds of theoretical modes were summarized and analyzed respectively．The importance of the gelled propellants combustion characteristic research was addressed．In addition， some proposals were given based on the research work．
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备注/Memo
收稿日期：2009—05—10；修回日期：2009—06-06。基金项目：国家自然科学基金(50576105)。 作者简介：丰松江(198l一)。男，博士研究生，研究领域为新型液体火箭发动机燃烧过程与燃烧不稳定性机理。
更新日期/Last Update:
1900-01-01