欧洲典型再入飞行测试技术分析

推进技术 ›› 2018, Vol. 39 ›› Issue (10): 2289-2296.

欧洲典型再入飞行测试技术分析

张云昊¹,白光辉¹,尤延铖²,付秋军¹,陈瞳¹

空间物理重点实验室，北京 100076,空间物理重点实验室，北京 100076,厦门大学航空航天学院，福建厦门 361005,空间物理重点实验室，北京 100076,空间物理重点实验室，北京 100076

发布日期:2021-08-15
作者简介:张云昊，女，硕士，高级工程师，研究领域为特种试验与测量技术。

Review of Europe Re-Entry Flight Test Technology

Science and Technology on Space Physics Laboratory，Beijing 100076，China,Science and Technology on Space Physics Laboratory，Beijing 100076，China,School of Aerospace Engineering，Xiamen University，Xiamen 361005，China,Science and Technology on Space Physics Laboratory，Beijing 100076，China and Science and Technology on Space Physics Laboratory，Beijing 100076，China

Published:2021-08-15

摘要/Abstract

摘要： 为深入认识大气再入气动物理参数飞行测试技术体系研究进展，概述了IXV，SHEFEX和EXPERT等典型欧洲再入飞行试验项目中所采用的特种环境飞行测试技术，并以EXPERT为主对其所搭载特种测试技术的目的、意义和技术概况进行了探讨，并对该领域技术研究提出了建议。

关键词: 航天器；大气再入；飞行测试；测量

Abstract: For further understanding of atmospheric reentry aerodynamic parameters flight test technical system，the special environment flight test technologies used on representative Europe re-entry flight test project，such as IXV，SHEFEX and EXPERT，have been studied. The objectives，significances and technology of the special environment flight test technologies on board of the EXPERT have been discussed. The proposals on technology research have been presented at last.

Key words: Spacecraft；Atmospheric reentry；Flight test；Measurement

张云昊,白光辉,尤延铖,付秋军,陈瞳. 欧洲典型再入飞行测试技术分析[J]. 推进技术, 2018, 39(10): 2289-2296.

ZHANG Yun-hao¹,BAI Guang-hui¹,YOU Yan-cheng²,FU Qiu-jun¹,CHEN Tong¹. Review of Europe Re-Entry Flight Test Technology[J]. Journal of Propulsion Technology, 2018, 39(10): 2289-2296.

参考文献

[1] 乐嘉陵. 吸气式高超声速技术研究进展[J]. 推进技术, 2010, 31(6): 641-649. (LE Jia-ling. Progress in Air-Breathing Hypersonic Technology[J]. Journal of Propulsion Technology, 2010, 31(6): 641-649.)
[2] 刘兴洲. 中国超燃冲压发动机研究回顾[J]. 推进技术, 2008, 29(4): 385-394. ( LIU Xing-zhou. Review of Scramjet Research in China[J]. Journal of Propulsion Technology, 2008, 29(4): 385-394.)
[3] 杨凯, 原志超, 朱强华, 等. 高超声速热化学非平衡钝体绕流数值模拟[J]. 推进技术, 2014, 35(12): 1585-1591. (YANG Kai, YUAN Zhi-chao, ZHU Qiang-hua, et al. Numerical Simulation of Hypersonic Thermochemical Nonequiliburium Blunt Body Flows[J].Journal of Propulsion Technology, 2014, 35(12): 1585-1591.)
[4] 刘健, 原志超, 杨凯, 等. 高超声速飞行器多层复杂热防护结构气-固耦合快速热分析方法[J]. 推进技术, 2016, 37(2): 227-234. (LIU Jian, YUAN Zhi-chao, YANG Kai, et al. Fast Algorithm of Coupled Flow-Thermal for Multi-Layered Complex TPS of Hypersonic Aircraft[J]. Journal of Propulsion Technology, 2016, 37(2): 227-234.)
[5] Le Jialing. Preliminary Study of Integrated Aero-Propulsive Performance of Vehicle with CFD and Experiments[R]. AIAA 2006-7982.
[6] Li Mailiang, Zhou Jin, GengHui, et al. Investigations on Function of Cavity in Supersonic Combustion Using OH PLIF[R]. AIAA 2004-3657.
[7] Tumino G, Mancuso S, Gallego J-M, et al. The IXV Experience, from the Mission Conception to the Flight Results[J]. Acta Astronautica, 2016, 124: 2-17.
[8] Roberto Angelini, Angelo Denaro. IXV Re-Entry Demonstrator: Mission Overview, System Challenges and Flight Reward[J]. Acta Astronautica, 2016, 124: 18-30.
[9] Klaus Hannemann. Hypersonic Flight and Re-Entry in Germany-Overview and Selected Projects[C]. San Fancisco: 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2011.
[10] Javier Bartolome Calvo, Thino Eggers. Application of a Coupling of Aerodynamics and Flight Dynamics to the SHEFEX I Flight Experiment[R]. AIAA 2011-2323.
[11] John Turner, Marcus H?rschgen, Josef Ettl, et al. SHEFEX 2 Development Status of the Vehicle and Sub-Systems for a Hypersonic Re-Entry Flight Experiment[C]. Bad Reichenhall: 19th ESA Symposium on European Rocket and Balloon Programmes and Related Research, 2009.
[12] The SHEFEX Team. SHEFEX II 2nd Flight within DLR’s Re-Entry Technology and Flight Test Program[EB/OL]. www.esaconferencebureau.com/docs/default-source/projectcode-docs/shefex-II-2nd -flight-within-dir’s-re-entry-technology-and-flight-test-program.pdf, 2016-08-01.
[13] JBarrio A M, Sudars M, Aulisio R, et al. EXPERT: The ESA Experimental Re-Entry Test-Bed[R]. AIAA 2011-6342.
[14] Massobrio F, Viotto R, Serpicob M, et al. EXPERT: An Atmospheric Re-Entry Test-Bed[J]. Acta Astronautica, 2007, 60: 974-985.
[15] Ottens H, Walpot L. Aerodynamic Environment and Flight Measurement Techniques of EXPERT[R]. AIAA 2006-8118.
[16] The Spaceflight101 Team. IXV-Intermediate Experimental Vehicle[EB/OL]. www.spacelight101.com/spacecraft/ixv-intermediate-experimental-vehicle.pdf, 2016-08-01.
[17] Ali Gülhan, Thomas Thiele, Frank Siebe. Challenges of the Instrumentation for High Speed Entry Vehicles[EB/OL]. www.solarsystem.nasa.gov/docs/2-Guelhan-Instrumentation.pdf, 2016-08-01.
[18] Francesca Cipollini, Jean-Marie Muylaert. European Activities on Advanced Flight Measurement Techniques for Hypersonic Space Vehicles[R]. AIAA 2006-3832.
[19] Herdrich G, L?hle S, Auweter-Kurtz M, et al. IRS Ground-Testing Facilities: Thermal Protection System Development, Code Validation and Flight Experiment Development[R]. AIAA 2004-2596.
[20] Muylaert J, Cipollini F, Walpot L, et al. Flight Experiments for Hypersonic Vehicle Development Expert[R]. ESA/RTO-EN-AVT-116, 2004.　　　　　　　　　　　　　*　收稿日期:2017-10-02；修订日期:2017-12-06。作者简介:张云昊,女,硕士,高级工程师,研究领域为特种试验与测量技术。E-mail: yunhaO₂004@sina.com(编辑:朱立影)