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先进混合动力火箭发动机燃料技术研究进展

于晓冬 高宏伟 胡楚睿 张伟 沈瑞琪

含能材料2025,Vol.33Issue(9):1005-1014,10.
含能材料2025,Vol.33Issue(9):1005-1014,10.DOI:10.11943/CJEM2025150

先进混合动力火箭发动机燃料技术研究进展

Research Progress on Advanced Hybrid Rocket Fuel

于晓冬 1高宏伟 1胡楚睿 1张伟 1沈瑞琪1

作者信息

  • 1. 南京理工大学化学与化工学院,江苏 南京 210094||南京理工大学空间推进技术研究所,江苏 南京 210094||微纳含能器件工业和信息化部重点实验室,江苏 南京 210094
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摘要

Abstract

Hybrid rocket motor is a thermochemical propulsion method that stores different phases of fuel and oxidizer separate-ly,which has the advantages of simple structure,low cost and adjustable thrust,making it possess wide applicability in military and commercial fields.However,the low regression rate and imbalance of mechanical properties restrict the development of hy-brid rocket engines.This review summarizes the composition,combustion characteristics,laws and key technologies for improv-ing combustion performance of typical hybrid rocket fuels,and analyzes the preparation methods and combustion performances of additive manufacturing fuels.Moreover,the future development directions and trends for advanced hybrid rocket motor fuels are also outlined,which provides insights and references for improving the performance of motors.

关键词

混合动力火箭发动机/退移速率/混合推进燃料/增材制造

Key words

hybrid rocket motor/regression rate/hybrid rocket fuel/additive manufacturing

分类

军事科技

引用本文复制引用

于晓冬,高宏伟,胡楚睿,张伟,沈瑞琪..先进混合动力火箭发动机燃料技术研究进展[J].含能材料,2025,33(9):1005-1014,10.

基金项目

国家自然科学基金(12074187) National Natural Science Foundation of China(No.12074187) (12074187)

含能材料

OA北大核心

1006-9941

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