航天推进技术研究院主办
[1]佘文学,刘晓鹏,刘凯.桑格尔空天飞行器技术途径分析与思考[J].火箭推进,2021,47(06):11-20.
SHE Wenxue,LIU Xiaopeng,LIU Kai.Analysis and thinking on technical approach of Sanger aerospace vehicle[J].Journal of Rocket Propulsion,2021,47(06):11-20.
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SHE Wenxue,LIU Xiaopeng,LIU Kai.Analysis and thinking on technical approach of Sanger aerospace vehicle[J].Journal of Rocket Propulsion,2021,47(06):11-20.
桑格尔空天飞行器技术途径分析与思考
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
47
期数:
2021年06期
页码:
11-20
栏目:
专刊
出版日期:
2021-12-31
- Title:
- Analysis and thinking on technical approach of Sanger aerospace vehicle
- 文章编号:
- 1672-9374(2021)06-0011-10
- 分类号:
- V475.3
- 文献标志码:
- A
- 摘要:
- 回顾了德国桑格尔两级入轨空天飞行器方案的研究概况,对其总体方案、推进系统、气动布局、结构热防护设计中的难点与关键问题开展了分析,并详细讨论了相关技术途径的可行性。借鉴桑格尔空天飞行器方案的经验与教训,分析了空天飞行器研究中面临的若干关键难点问题,提出了未来空天飞行器发展路线与实施建议。
- Abstract:
- The research situation of German Sanger two-stage-to-orbit aerospace vehicle is reviewed. The difficulties and key issues in conceptual design,propulsion system,aerodynamic layout and structural thermal protection design are analyzed,and the feasibility of relevant technical approaches is discussed in detail. Based on the experience and lessons of Sanger aerospace vehicle scheme,this paper analyzes the key technology issues in the research of aerospace vehicle,and proposes the development route and implementation suggestions of aerospace vehicle in the future,so as to provide reference direction for the follow-up development of aerospace vehicle.
参考文献/References:
[1] 包为民,汪小卫,董晓琳. 航班化航天运输系统对动力的发展需求与技术挑战[J].火箭推进,2021,47(4):1-5.
BAO W M,WANG X W,DONG X L. Development demands and challenges of propulsion technology for space transportation system in airline-flight-mode[J].Journal of Rocket Propulsion,2021,47(4):1-5.
[2] 本特利. 空天飞行器:从飞机场到航天港[M].张红文,关成启,佘文学,译.北京:北京理工大学出版社,2015.
[3] SACHER H K P W.可重复使用空间运输系统[M].魏毅寅,张红文,王长青,译.北京:国防工业出版社,2015.
[4] 王长青. 空天飞行技术创新与发展展望[J].宇航学报,2021,42(7):807-819.
[5] DENEU F,MALASSIGNE M,LE-COULS O,et al.Promising solutions for fully reusable two-stage-to-orbit configurations[J].Acta Astronautica,2005,56(8):729-736.
[6] FUJII K,ISHIMOTO S. Research activities to realize advanced space transportation system[C]//16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. Reston,Virginia:AIAA,2009.
[7] EKLUND D. Quicksat:a two stage to orbit reusable launch vehicle utilizing air breathing propulsion for responsive space access[C]//Space 2004 Conference and Exhibit. Reston,Virginia:AIAA,2004.
[8] MINAMI Y,ISHIMOTO S,MORI T,et al.Design study on a small-sized partially reusable launch system[C]//AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. Reston,Virginia:AIAA,2005.
[9] 佘文学,刘凯,乔鸿. 组合动力空天飞行器制导技术发展分析[J].战术导弹技术,2020(5):52-65.
[10] 唐硕,龚春林,陈兵. 组合动力空天飞行器关键技术[J].宇航学报,2019,40(10):1103-1114.
[11] HOGENAUER E,KOELLE D E. SANGER:the German aerospace vehicle program[C]//AlAA First National Aerospace Planes Conference. Reston,Virginia:AIAA,1989.
[12] AFANASEV V A,DEGTYAREV G L,MESHCHANOV A S. Reusable space transportation system[J].Russian Aeronautics,2018,61(3):325-330.
[13] DIETER J,SIEGFRIED W. Basic research on TSTO[Z].2001.
[14] SACHER P. The engineering design of engine/airframe integration for the SANGER fully reusable space transportation system [EB/OL].https://xueshu.baidu.com/usercenter/paper/show?paperid=3b9a669a48e950ea179 a59456ed682f7,2010.
[15] KOELLE D. Advanced two-stage launch vehicle concepts(Saenger)[C]//26th Joint Propulsion Conference. Reston,Virginia:AIAA,1990.
[16] KUCZERA H,SACHER P,KRAMMER P. SANGER and the German hypersonics technology programme,status[R].IAF-91-198.
[17] 金捷,陈敏,刘玉英. 涡轮基组合循环发动机[M].北京:国防工业出版社,2019.
[18] WEINGERTNER S. SAENGER:the reference concept of the German hypersonics technology program[C]//5th International Aerospace Planes and Hypersonics Technologies Conference. Reston,Virigina:AIAA,1993.
[19] KUCZERA H,HELMUT H. The German hypersonics technology programme[C]//AlAA 4th International Aerospace Planes Conference. Reston,Virginia:AIAA,1992.
[20] TROLLHEDEN S,STREIFINGER H. Secondary power system study for the SAENGER first stage vehicle[C]//5th International Aerospace Planes and Hypersonics Technologies Conference. Reston,Virigina:AIAA,1993.
备注/Memo
收稿日期:2021-08-28 修回日期:2021-09-16
基金项目:国家自然科学基金(61603363)
作者简介:佘文学(1966—),男,博士,研究员,副总设计师,研究领域为可重复使用空天飞行器总体设计。
更新日期/Last Update:
1900-01-01