YANG Ya-zheng, YANG Jia-ling, FANG Dai-ning. Research Progress on the Thermal Protection Materials and Structures in Hypersonic Vehicles[J]. Applied Mathematics and Mechanics, 2008, 29(1): 47-56.
Citation: YANG Ya-zheng, YANG Jia-ling, FANG Dai-ning. Research Progress on the Thermal Protection Materials and Structures in Hypersonic Vehicles[J]. Applied Mathematics and Mechanics, 2008, 29(1): 47-56.

Research Progress on the Thermal Protection Materials and Structures in Hypersonic Vehicles

  • Received Date: 2007-10-07
  • Rev Recd Date: 2007-10-29
  • Publish Date: 2008-01-15
  • Hypersonic vehicles represent future trends of military equipments and play an important role in future war. Thermal protection materials and structures, which relate to the safety of hypersonic vehicles, are one of the most key techniques in design and manufacture of hypersonic vehicles. Among these materials and structures, such as metallic temperature protection structure, the a-high temperature ceramics and carbon/ carbon composites are usually adopted in design. The recent progresses of research and application of ultra-high temperature materials in preparation, oxidation resistance, mechanical and physical characterization were summarized.
  • loading
  • [1]
    Moses Paul L,Rausch Vincent L,Nguyen Luat T,et al.NASA hypersonic flight demonstrators-overview, status and future plans[J].Acta Astronautica,2004,55(3/4):619-630. doi: 10.1016/j.actaastro.2004.05.045
    [2]
    Jay Miller. The X-planes X-1 to X-29[J].Specialty Press,Marine on St Croix,MN,1983,(4):10-13.
    [3]
    Bohon H L, Shideler J L. Radioactive metallic thermal protection systems: a status report[J].Journal of Spacecraft and Rockets,1977,12(10):626-631.
    [4]
    Shideler J L, Kelly H N, Avery D E. Multiwall TPS-an emerging concept[J].Journal of Spacecraft and Rockets,1982,19(4):7-8.
    [5]
    Blair W, Meaney J E,Rosenthal H A. Fabrication of prepackaged super alloy honeycomb thermal protection system panels[R]. NASA-TP-3257,1993,(3):5-7.
    [6]
    Gorton M P, Shideler J L, Web G L. Static and aero thermal tests of a super alloy honeycomb prepackaged thermal protection system[R]. NASA-TP-3257,1993, (3):2-3.
    [7]
    Cunnington G R, Zierman C A. Performance of multi-layer insulation systems for temperatures to 700K[R ]. NASA CR-907,1967210,1967.
    [8]
    Keller K, Hoffmann M, Zorner W,et al.Application of high temperature multilayer insulations[J].Acta Astronautica,1992,26(6):451-458. doi: 10.1016/0094-5765(92)90073-R
    [9]
    Daryabeigi Kamran. Thermal analysis and design of multi-layer insulation for reentry aerodynamic heating[R]. AIAA 2001-2834.
    [10]
    Daryabeigi Kamran. Effective thermal conductivity of high temperature insulations for reusable launch vehicles[R]. NASA TM-1999-20892.
    [11]
    Sullins Alan D, Daryabeigi Kam ran.Effective thermal conductivity of high porosity open cell Nickel foam[R]. AIAA 2001-2819.
    [12]
    Daryabeigi Kamran.Heat transfer in high temperature fibrous insulation[R]. AIAA 2002-3332.
    [13]
    Daryabeigi Kamran. Analysis and testing of high temperature fibrous insulation for reusable launch vehicles[R]. AIAA 99-1044,1999.
    [14]
    Blosser M L. Development of metallic thermal protection systems for the reusable launch vehicle[R]. NASA Technical Memorandum,110 296,1996.
    [15]
    姚草根,吕宏军,贾新潮,等.金属热防护系统材料与结构研究进展[J].宇航材料工艺,2005,35(2):10-13.
    [16]
    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,2002,256(2):21-26.
    [17]
    关春龙,李,赫晓东.可重复使用热防护系统防热结构及材料的研究现状[J].宇航材料工艺,2003,33(6):7-11.
    [18]
    曹义,程海峰,肖加余,等.美国金属热防护系统研究进展[J].宇航材料工艺,2003,33(3):9-12.
    [19]
    韩杰才,陈贵清,孟松鹤,等.新型ARMOR热防护系统[J].宇航学报,2004,25(3):350-353.
    [20]
    赵颖.2000年世界运载器发展综述[J].导弹与航天运载技术,2001,249(1):16-22.
    [21]
    Myers D E,Martin C J,Blosser M L. Parametric weight comparison of current and proposed thermal protection system (TPS) concepts[A].In:33rd AIAA Thermophysics Conference[C].AIAA 93-3459,Norfolk,Virginia:June 28-July 1,1999.
    [22]
    Cowart K, Olds J.Integrating aeroheating and TPS into conceptual RLV design[A].In:9th International Space Planes and Hypersonic Systems and Technologies Conference[C].AIAA 99-4806,Norfolk,VA:November 1-5,1999.
    [23]
    Brewer W D,Wallace Terryl A,Bird R Keith,et al.Alloys and coating development for metallic TPS for reusable launch vehicles[A].In:2000 National Space Missile Materials Symposium[C].San Diego.California:February 28-March 2, 2000.
    [24]
    Buckley J D,Ediel D D.Carbon-Carbon Materials and Composites[M].New York:Noyes Publications,1993.
    [25]
    Savage G.Carbon/Carbon Composites[M].London:Chapman & Hall,1993,198-209.
    [26]
    Walker Jr P L.Carbon em dash an old but new material[J].Carbon,1972,10(4):369-382.
    [27]
    Lavruquere S,Blanchard H, Pailler R,et al.Enhancement of the oxidation resistance of interfacial area in C/C composites. Part Ⅱ. Oxidation resistance of B-C, Si-B-C and Si-C coated carbon preforms densified with carbon[J].Journal of the European Ceramic Society,2002,22(7):1011-1021. doi: 10.1016/S0955-2219(01)00411-3
    [28]
    崔红, 苏君明,李瑞珍,等.添加难熔金属碳化物提高碳/碳复合材料抗烧蚀性能的研究[J].西北工业大学学报,2000,4(18):669-673.
    [29]
    闫桂沈,王俊,苏君明,等.难熔金属碳化物改性基体对碳/碳复合材料抗氧化性能的影响[J].炭素,2003,114(2):3-6.
    [30]
    朱小旗,杨峥,康沫狂,等.基体改性碳/碳复合材料抗氧化影响规律探析[J].复合材料学报,1994,11(2):107-111.
    [31]
    罗瑞盈,李东生.提高碳/碳复合材料抗氧化性能的一种新途径[J]. 宇航学报,1998,19(1):95-98.
    [32]
    Park Soo jin,soe Min kang.The effects of Mosi2 on the oxidation behavior of carbon/carbon composites[J].Carbon,2001,39(8):1229-1235. doi: 10.1016/S0008-6223(00)00248-7
    [33]
    Jashi A, Lee J S. Coating with particulate dispersions for high temperature oxidation protection of carbon and C-C composites[J].Composites A,1997,28(2):181-189. doi: 10.1016/S1359-835X(96)00111-X
    [34]
    成来飞, 张立同, 韩金探.液相法制备碳-碳Si-Mo防氧化涂层[J].高技术通信,1996,6(4):17-20.
    [35]
    成来飞,张立同,徐永东,等.液相法制备碳-碳Si-W防氧化涂层[J]. 硅酸盐通报,1997,25(5):537-541.
    [36]
    曾燮榕, 李贺军, 张建国,等.碳/碳复合材料防护涂层的抗氧化行为研究[J].复合材料学报,2000,17(2):42-45.
    [37]
    HUANG Jian-feng,ZENG Xie-rong,LI He-jun,et al.Al2O3-mullite-SiC- Al4 SiC4 multi-composition coating for carbon / carbon composites[J].Materials Letters,2004,58(21):2627-2630. doi: 10.1016/j.matlet.2004.03.046
    [38]
    HUANG Jian-feng,ZENG Xie-rong,LI He-jun,et al.ZrO2-SiO2 gradient multi-layer oxidation protective coating for SiC coated carbon/carbon composites[J].Surface & Coating Technology,2005,190(2/3):255-259.
    [39]
    Cairo C A A,Graca M L A,Silva C R M,et al.Functionally gradient ceramic coating for carbon/carbon anti-oxidation protection[J].Journal of European Ceramic Society,2001,21(3):325-329. doi: 10.1016/S0955-2219(00)00191-6
    [40]
    Buchanan F J,Little J A.Particulate containing glass sealants for carbon-carbon composites[J].Carbon,1996,31(4):649-654.
    [41]
    Strife J R.Ceramic coating for carbon-carbon composites[J].Ceramic Bulletin,1988,67(2),369-374.
    [42]
    WU Tsung-ming,WU Yung-rong.Methodology in exploring the oxidation behavior of coated-carbon/carbon composites[J].Journal of Materials Science,1994,29(5):1260-1264. doi: 10.1007/BF00975073
    [43]
    Westwood M E,Webster J D,Day R J,et al.Oxidation protection for carbon fiber composites[J].Journal of Materials Science,1996,31(6):1389-1397. doi: 10.1007/BF00357844
    [44]
    Eckel A J, Bradt R C.Thermal expansion of laminated, woven, continuous ceramic fiber/chemical-vapor-infiltrated silicon carbide matrix composites[J].Journal of American Ceramic Society,1990,73(5):1333-1338.
    [45]
    Rudy E. Compendium of phase diagram data: ternary phase equilibria in transition metal-boron-carbon-silicon systems Part 5—air force materials laboratory, wright -patterson air force base[R]. Ohio,1969.
    [46]
    Kaufman L, Clougherty E V.Investigation of boride compounds for very high temperature applications[R]. RTD-TRD-N63-4096, Part Ⅲ,Cambridge, MA:ManLabs Inc,March 1966.
    [47]
    Clougherty E V,Kalish D, Peters E T.Research and development of refractory oxidaton resistant diborides[R]. AFML-TR-68-190,Cambridge, MA:ManLabs Inc,1968.
    [48]
    Kaufman L, Nesor H.Stability characterization of refractory materials under high velocity atmospheric flight conditions[R]. Part Ⅲ,Vol Ⅲ, AFML-TR-69-84,Cambridge, MA:ManLabs Inc,1970.
    [49]
    Mcclaine L A.Thermodynamic and kinetic studies for a refractory materials program[R]. Report ASD/TDR/62/204, Part I,USA:Jan l, 1962.
    [50]
    Berkowitz-Mattuck J B.Kinetics of oxidation of refractory metals and alloys at 1000-2000℃[R]. Technical Report ASDTDR-62-203, AFML, WPAFB, OH, 1962/1963.
    [51]
    Peter T B, Shaffer. An Oxidation resistant boride composition[J].American Ceramic Society Bulletin,1962,41(2):96-99.
    [52]
    Pastor H, Meyer R.Study of the effect of additions of silicides of some group IV-VI transition metals on sintering and high-temperature oxidation resistance of titanium and zirconium borides[J].Revue Internationale des Hautes Temperatures et des Refractaires,1974,11(1):41-45.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (3068) PDF downloads(1365) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return