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[1]张 楠,孙慧娟.低温液体火箭发动机重复使用技术分析[J].火箭推进,2020,46(06):1-12.
　ZHANG Nan,SUN Huijuan.Analysis on the reusable cryogenic liquid rocket engine technology[J].Journal of Rocket Propulsion,2020,46(06):1-12.
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低温液体火箭发动机重复使用技术分析

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 46 期数: 2020年06期 页码: 1-12 栏目: 专注与论述 出版日期: 2020-12-31
Title:
Analysis on the reusable cryogenic liquid rocket engine technology
文章编号:
1672-9374(2020)06-0001-12
作者:
张 楠; 孙慧娟
(北京航天动力研究所,北京 100076)
Author(s):
ZHANG Nan; SUN Huijuan
(Beijing Aerospace Propulsion Institute, Beijing 100076,China)
关键词:
重复使用技术;  重复使用运载器;  低温液体火箭发动机;  指标体系;  推进剂组合
Keywords:
reusable technology;  reusable launch vehicle;  cryogenic liquid rocket engine;  guideline system;  propellant combination
分类号:
V434
文献标志码:
A
摘要:
为降低一次性运载火箭发射成本,宇航界一直在致力于研制像飞机一样可以多次自由进出太空的重复使用运载器。占全箭成本三分之一的发动机,是重复使用运载器研究的重要部分。在已获得的研究成果基础上,分析国内外重复使用技术发展特点,指出液体火箭发动机是近期实现运载器重复使用的现实动力方案,并据此初步确立发动机重复使用技术指标体系和推进剂组合,提出发动机重复使用关键技术。
Abstract:
There has been increasing attention payed to the reusable launch vehicle, because it has the potential to reduce the cost of access to space.The rocket engine cost accounts for one-third of the cost of a rocket.The engine reusable performance is important for the reusable launch vehicle.Based on previous studies, present study analyzed the reusable technical developing trends in domestic and abord, and then suggest using the cryogenic liquid rocket engine as the propulsion of the reusable launch vehicle is a possible approach in the near future.This paper built the preliminary guideline system of reusable engines, and suggested the key technologies.

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备注/Memo

收稿日期:2019-11-08; 修回日期:2020-04-07 作者简介:张楠(1960—),男,研究员,研究领域为低温液体火箭发动机

更新日期/Last Update: 1900-01-01