航天推进技术研究院主办
[1]杨思锋,段 娜,张登攀,等.液体火箭发动机虚拟试验与仿真技术应用[J].火箭推进,2021,47(04):87-95.
YANG Sifeng,DUAN Na,ZHANG Dengpan,et al.Summary of virtual test and simulation technology application in LRE field[J].Journal of Rocket Propulsion,2021,47(04):87-95.
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YANG Sifeng,DUAN Na,ZHANG Dengpan,et al.Summary of virtual test and simulation technology application in LRE field[J].Journal of Rocket Propulsion,2021,47(04):87-95.
液体火箭发动机虚拟试验与仿真技术应用
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
47
期数:
2021年04期
页码:
87-95
栏目:
测控与试验
出版日期:
2021-08-31
- Title:
- Summary of virtual test and simulation technology application in LRE field
- 文章编号:
- 1672-9374(2021)04-0087-09
- 关键词:
- 仿真验证 虚拟试验 液体火箭发动机
- 分类号:
- V433
- 文献标志码:
- A
- 摘要:
- 阐述了虚拟试验与仿真验证技术的基础理论,列举了美国喷气实验室、美国马歇尔空间飞行中心、美国肯尼迪空间中心、美国格林研究中心、俄罗斯科学试验中心、美国斯坦尼斯研究中心、德国DLR中心、日本Kakuda空间推进中心、法国宇航局等液体火箭发动机研制试验机构在虚拟试验与仿真领域的研究应用案例。分析了其应用成果均以成熟产品的形式推广应用,同时对比了我国在该领域的应用产品。最后综述了本项技术的发展趋势和试验台应用与相关研究的建议。通过总结分析可知国外的液体火箭发动机仿真工作覆盖面广、可信度高,从系统级到部件级的全工作过程都可以实时精准模拟,所有模型都经过了真实试车或飞行数据的校验和修正,为发动机试验领域实施和应用虚拟试验与仿真平台提供了技术参考。
- Abstract:
- This article describes the fundamental theory of virtual test and simulation verification technology,including the application cases of Jet Laboratory(US),Marshall Space Flight Center(US),Kennedy Space Center(US),Green Research Center(US),Russian Science Test Center,Stennis Research Center(US),DLR Center(Germany),Kakuda Space Propulsion Center(Japan),French Aerospace Agency and other liquid rocket engine development and test institutions in the field of virtual test and simulation research.Their application results are promoted and applied in the form of mature products,and the application products of China in this field are compared.Finally,the development trend of this technology,test bed application and related research suggestions are reviewed.Through the summary and analysis,it can be seen that the simulation work of foreign liquid rocket engines has wide coverage and high credibility,and the whole working process from the system level to the component level can be accurately simulated in real time.All models have been verified and corrected by real test runs or flight data, providing technical references for the implementation and application of virtual test and simulation platforms in the field of engine testing.
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备注/Memo
收稿日期:2019-07-25
基金项目:中国航天科技集团自主创新课题
作者简介:杨思锋(1966—),男,研究员,研究领域为液体火箭发动机试验与测试。
更新日期/Last Update:
1900-01-01