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金属热防护系统材料与结构研究进展 被引量:17

Development of Metallic Thermal Protection System
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摘要 简要综述了金属热防护系统的国外研究进展,重点介绍了美国高温合金热防护系统材料与结构以及钛合金热防护材料与结构的研究概况,并对国内情况作了一些简介。指出金属热防护系统是下一代重复使用运载器大面积表面热防护的第一方案。 The development of the foreign metallic thermal protection system (TPS) is briefly reviewed. The material and structure of superalloy metallic TPS and titanium alloy metallic TPS in USA is introduced in detail. And the development of the domestic metallic TPS is briefly introduced. It is indicated that metallic TPS is the No 1 blue print of the acreage TPS for the next generation reusable launch vehicle.
出处 《宇航材料工艺》 CAS CSCD 北大核心 2005年第2期10-13,共4页 Aerospace Materials & Technology
关键词 热防护系统 研究进展 结构 金属 重复使用运载器 热防护材料 研究概况 高温合金 钛合金 Metallic thermal protection system, Reusable launch vehicle, Thermal protection structure
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参考文献25

  • 1夏德顺.重复运载器金属热防护系统的述评[J].导弹与航天运载技术,2002(2):21-26. 被引量:31
  • 2韩鸿硕.国外航天器防热系统和材料的应用研究现状[J].宇航材料工艺,1994,24(6):1-4. 被引量:14
  • 3Miller Jay. The X - planes: X - 1 to X - 29. Specialty Press, Marine on St. Croix, MN, 1983.
  • 4Scoville C L, Gorsuch P D. Thermal protection systems for the space shuttle. In: Astronautical research 1970, proceedings of the ⅩⅪst congress of the intermational astronautical federation, Konstanz, West Germany, 1970, Amsterdam: North Holland Publishing Co. , 1971: 424 ~443.
  • 5Groninger B V. Titanium and superalloy heat shield design for space shuttle application. In: Technology today and tomorrow, canaveral counicl of technical societies, 8th Space Congress, Cocoa Beach, Fla., Proceedings, 1971;1(7): 1~20.
  • 6Bohon H L,Shideler J L,Rummler D R. Radiative metallic thermal protection systems: a status report. Journal of Spacecraft and Rockets, 1977; 12(10): 626 ~631.
  • 7Shideler J L, Kelly H N, Avery D E, Blosser M L,Adelman H M. Multiwall TPS-An emerging concept. Journal of Spacecraft and Rockets, 1982; 19(4): 7 ~8.
  • 8Blair W, Meaney J E,Rosenthal H A. Fabrication of prepackaged superalloy honeycomb thermal protection system (TPS) panels. NASA-CR-3755,1985:2 ~40.
  • 9Gorton M P, Shideler J L,Web G L. Static and aerothermal tests of a supperalloy honeycomb prepackaged thermal protection system. NASA-TP-3257, 1993;(3): 1 ~50.
  • 10Blosser M L, Martin C J, Daryabeigi K, Poteet C C.Reusable metallic thermal protection systems development. In:Proceedings of the 3rd European Workshop on thermal protection systems, ESTEC, 1998: 165~ 176.

二级参考文献12

  • 1[1]Freeman Jr D C et al.Reusable launch vehicle technology program.47th IAG,1996-10:5
  • 2[2]Healy T J et al.Key technologies are being developed for the X-33/RLV.AIAA-95-3608,1995-09:1~12
  • 3[3]Myers D E et al.Parametric weight comparison of current and proposed thermal protection system(TPS) concepts.AIAA-99-3459,1999:1~11
  • 4[4]Vaughn R L,King R E.Space shuttle: a triumph in manufacturing.1985,5:176~178
  • 5[5]Multiwall TPS--an emerging concept.Journal of Spacecraft and Rockets,1982,19(4): 358~365
  • 6[6]Bohon H L et al.Radioactive metallic thermal protection system: A status report.Journal of Spacecraft and Rockets,1977,14(10):626~631
  • 7[7]Leonard David.X-33 flight test vehicle to use metallic panels.Space News,1996-09:6
  • 8[8]Frank Bokulich.Heat shield ready for X-33.Aerospace Engineering,1999-04:23~24
  • 9[9]Sawyer J W et al.Aerothermal test of metallic TPS for X-33 RLV.Europe Research Workshop,1998:1~2
  • 10[10]Blosser M L.Development of metal TPS for the RLV.A97-26123,1996.

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同被引文献270

引证文献17

二级引证文献188

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