航天推进技术研究院主办
[1]陈明亮,刘昌国,徐 辉,等.远征三号上面级轨控发动机研制及在轨验证[J].火箭推进,2020,46(03):11-18.
Hui,WU Erlong.Development and in-orbit verification of orbit-control engine in YZ-3 upper stage[J].Journal of Rocket Propulsion,2020,46(03):11-18.
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Hui,WU Erlong.Development and in-orbit verification of orbit-control engine in YZ-3 upper stage[J].Journal of Rocket Propulsion,2020,46(03):11-18.
远征三号上面级轨控发动机研制及在轨验证
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
46
期数:
2020年03期
页码:
11-18
栏目:
研究与设计
出版日期:
2020-06-25
- Title:
- Development and in-orbit verification of orbit-control engine in YZ-3 upper stage
- 文章编号:
- 1672-9374(2020)03-0011-08
- 分类号:
- V439.7
- 文献标志码:
- A
- 摘要:
- 综述了国内外上面级及其轨控发动机技术发展情况。基于远征三号上面级的任务特点,提出了5 000 N轨控发动机技术方案,着重介绍了5 000 N发动机的地面试验和首次飞行应用情况,总结了远征三号上面级轨控发动机研制经验,供类似火箭发动机研制参考。远征三号上面级5 000 N发动机采用挤压式推进剂供应系统、直流式喷注器、再生冷却方案和复合材料喷管延伸段,具有结构简单、多次启动能力强、双向摇摆角度大等优势,于2018年12月29日进行了首次飞行应用
- Abstract:
- The technical development of the upper stage and its orbit-control engine at home and abroad is reviewed in this paper. Based on the mission characteristics of YZ-3 upper stage, the technical scheme of 5 000 N upper stage engine is put forward, focusing on its ground tests and the first flight application. The development experience of YZ-3 upper stage engine is summarized for the reference of similar rocket engine development. Since the 5 000 N upper stage engine of YZ-3 adopts the extruded propellant supply system, orifice injector,regenerative cooling and C/SiC composite nozzle,it has the advantages of simple structure,multiple ignitions,large scale two-way swing. The first application flight was carried on December 29,2018
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备注/Memo
收稿日期:2019-08-23; 修回日期:2019-10-14
基金项目:上海市空间发动机工程技术研究中心资助项目(17DI2280800)
作者简介:陈明亮(1986—),男,硕士,高级工程师,研究领域为液体火箭发动机设计研发
更新日期/Last Update:
2020-06-25