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[1]韩 伟,王永忠,单世群,等.氧化亚氮基氧燃一体化推进剂及推进系统研究进展[J].火箭推进,2020,46(05):1-9.
　HAN Wei,WANG Yongzhong,SHAN Shiqun,et al.Research progress of nitrous-oxide-based oxidizer-fuel integrated propellant and propulsion system[J].Journal of Rocket Propulsion,2020,46(05):1-9.
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氧化亚氮基氧燃一体化推进剂及推进系统研究进展

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 46 期数: 2020年05期 页码: 1-9 栏目: 专论与综述 出版日期: 2020-10-20
Title:
Research progress of nitrous-oxide-based oxidizer-fuel integrated propellant and propulsion system
文章编号:
1672-9374(2020)05-0001-09
作者:
韩 伟; 王永忠; 单世群; 杜宗罡; 朱成财; 于忻立
(西安航天动力试验技术研究所,陕西 西安 710100)
Author(s):
HAN Wei; WANG Yongzhong; SHAN Shiqun; DU Zonggang; ZHU Chengcai; YU Xinli
(Xi’an Aerospace Test Technology Research Institute, Xi’an 710100,China)
关键词:
氧化亚氮;  一体化推进剂;  推进系统;  燃烧特性
Keywords:
nitrous oxide;  integrated propellant;  propulsion system;  combustion characteristic
分类号:
V511
文献标志码:
A
摘要:
氧化亚氮基氧燃一体化推进剂因具有无毒、高比冲、宽温幅等诸多优异性能,受到各航天科研工作者的广泛关注。美国、荷兰、英国、德国、中国在该推进剂及其推进系统研究方面开展了许多卓有成效的工作。综述了2016年以来国内外在氧化亚氮基氧燃一体化推进剂的配方体系、发动机设计、燃烧过程及防回火特性等方面的研究进展,结合我国实际现状,提出了下一步开展氧化亚氮基氧燃一体化推进剂及推进系统的建议。
Abstract:
Nitrous-oxide-based oxidizer-fuel integrated propellant has been widely concerned by many aerospace scientists due to its excellent properties such as non-toxic, high specific impulse and wide temperature range.The United States, the Netherlands, the United Kingdom, Germany and China have carried out a lot of successful work on the propellant and its propulsion system.In this paper, the research progress in the formula system, engine design, combustion process and anti-tempering characteristics of nitrous-oxide-based oxidizer-fuel integrated propellant at home and abroad since 2016 is reviewed.Combined with the actual situation in China, some suggestions for the further development of nitrous-oxide-based oxidizer-fuel integrated propellant and propulsion system are put forward.

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备注/Memo

收稿日期:2020-02-29; 修回日期:2020-04-13
基金项目:军委科技委创新特区项目(18-H863-03)
作者简介:韩伟(1975—),男,硕士,研究员,研究领域为液体推进剂

更新日期/Last Update: 2020-10-20