飞行器典型热密封结构

宇航材料工艺 , 2013, 43(1): 20-25.

飞行器典型热密封结构

李凡 ^1, , 王树浩 ^2, , 陈江涛 ^3, , 赵光辉 ^4, , 于焕光 ^5,

1.航天材料及工艺研究所,北京 100076

2.二炮驻首都航天机械公司军事代表室,北京 100076

3.航天材料及工艺研究所,北京 100076

4.二炮驻首都航天机械公司军事代表室,北京 100076

5.航天材料及工艺研究所,北京 100076

关键词：可重复使用飞行器 , 高超声速飞行器 , 热密封 , 密封结构

Typical High-Temperature Seal Structur of Reusable and Hypersonic Vehicles

对航天飞机、X-38和X-51等飞行器的热密封结构进行了综合评述.分析了机身TPS、机身开口部位及控制面三个安装部位的热密封结构特点,综述了其热密封组件的研究历程和使用现状.

参考文献

[1]	Bruce Dr;Steinetz M .Seal technology for hypersonic vehicles and propulsion systems:an overview[OL].http://scitech.calt.casc
[2]	John Celand;Francesco Iannetti .Thermal protection system of the space shuttle[NASA Contractor Report 4227][R].,1989.
[3]	Curry D M;Latchem J W;Whisenhunt G B .Space shuttle orbitor leading edges structural subsystem development[AIAA-83-0483][R].Reno,1983.
[4]	McBride D U.Subsurface flow considerations in thermal protection design[A].,1986
[5]	Finkbeiner Joshua;Dunlap Pat;Steinetz Bruce .nvestigations of shuttle main landing gear door environmental seals[NASA/TM-2005-0213860][R].,2005.
[6]	Cooper Griffin Snapp .Ecaluation of space shuttle tile subnominal bonds[D].University of Kansas,2000.
[7]	Fu J H;Graves G R .Thermal environments for space Shuttle payloads[AIAA-85-6058][R].,1985.
[8]	McAnally Bill M .Space Shuttle orbiter payload bay door mechanisms[NASA/TM-2001-210338][R].
[9]	Jeffrey De Mange;Shawn Taylor .Overview of CEV thermal protection system seal development[NASA/CP-2009-215677][R].,2009.
[10]	Jeffrey De Mange .Advanced control surface seal development for future space vehicles[NASA/CP-2004-212963][R].,2004.
[11]	Patrick H. Dunlap Jr.;Bruce M. Steinetz;Donald M. Curry;Jeffrey J. DeMange;H. Kevin Rivers;Su-Yuen Hsu .Investigations of a Control Surface Seal for Reentry Vehicles[J].Journal of spacecraft and rockets,2003(4):570-583.
[12]	Dunlap Patrick H;Steinetz Bruce M .Rudder/Fin seal investigations for the X-38 Re-Entry vehicle[NASA/TM-2000-210338][R].
[13]	Taylor Shawn C;Demange Jeffrey J .Evaluation of high temperature knitted spring tubes for structural seal applications[NASA/TM-2004-213183][R].,2004.
[14]	Glass David E;Ray Dirling;Harold Croop et al.Materials development for hypersonic flight vehicles[AIAA-2006-8122][R].

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飞行器典型热密封结构

Typical High-Temperature Seal Structur of Reusable and Hypersonic Vehicles

参考文献