欢迎登录材料期刊网

材料期刊网

高级检索

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.

参考文献

[1] 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(06):1-4.
[2] Blosser M L.Development of metallic thermal protection systems for the reusable launch vehicle[J].NASA Technical Memorandum 110296,1996:1-22.
[3] 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(02):21-26.
[4] Miller Jay.The X - planes: X - 1 to X - 29. Specialty Press[M].Marine on St. Croix, MN,1983
[5] Scoville C L;Gorsuch P D.Thermal protection systems for the space shuttle[A].Amsterdam: North Holland Publishing Co,1971:424-443.
[6] Groninger B V.Titanium and superalloy heat shield design for space shuttle application[A].Cocoa Beach ,Fla, ,Proceedings,1971:1-20.
[7] Bohon H L;Shideler J L;Rummler D R .Radiative metallic thermal protection systems:a status report[J].Journal of Spacecraft and Rockets,1977,12(10):626-631.
[8] Shideler J L;Kelly H N;Avery D E;Blosser M L Adelman H M .Multiwall TPS-An emerging concept[J].Journal of Spacecraft and Rockets,1982,19(04):7-8.
[9] Blair W;Meaney J E;Rosenthal H A .Fabrication of prepackaged superalloy honeycomb thermal protection system (TPS) panels[R].NASA-CR-3755,1985.
[10] Gorton M P;Shideler J L;Web G L .Static and aerothermal tests of a supperalloy honeycomb prepackaged thermal protection system[R].NASA-TP-3257,1993.
[11] Blosser M L;Martin C J;Daryabeigi K;Poteet C C.Reusable metallic thermal protection systems development[A].ESTEC,1998:165-176.
[12] Wells R R .Fabrication of titanium thermal protection system panels by the Nor-Ti-Bond process[R].NASA -CR-123536,1971.
[13] Blair W;Meaney J E Jr;Rosenthal H A .Design and fabrication of titanium multi-wall thermal protection system (TPS) test panels[R].NASA - CR - 159241,1980.
[14] Blair W;Meaney J E;Rosenthal H A .Re-design and fabrication of titanium multi-wall thermal protection system (TPS) test panels[R].NASA-CR-172247,1984.
[15] Blair W .Fabrication of titanium multiwall thermal protection system (TPS) curved panel[R].NASA - CR - 165754,1981.
[16] Baumgartner R I.VentureStar a revolutionary space transprotaion launch system[A].,1998:867-874.
[17] Bouslog S A;Moore B.X -33 metallic TPS tests In NASA-larc high temperature tunnel[J].Thermophysics Session ALAA 37th Aerospace Sciences Meeting,1999:1-15.
[18] Bloaser M.Thermal protection systems for reusable launch vehicles.Thermal & Fluids Analysis Workshop[M].Hampton ,VA,2003
[19] John T. Dorsey;Carl C. Poteet;Kathryn E. Wurster;Roger R. Chen .Metallic Thermal Protection System Requirements, Environments, and Integrated Concepts[J].Journal of spacecraft and rockets,2004(2):162-172.
[20] M. L. Blosser;R. R. Chen;I. H. Schmidt;J. T. Dorsey;C. C. Poteet;K. Bird;K. E. Wurster .Development of Advanced Metallic Thermal-Protection-System Prototype Hardware[J].Journal of spacecraft and rockets,2004(2):183-194.
[21] Brewer W D;Wallace T A;Bird K R;Sankaran S N.Alloys and coating development for metallic TPS for reusable launch vehicles[A].San Diego, California,2000
[22] R. Keith Bird;Terryl A. Wallace;Sankara N. Sankaran .Development of Protective Coatings for High-Temperature Metallic Materials[J].Journal of spacecraft and rockets,2004(2):213-220.
[23] Buursink J.Status of the delft aerospace RE-entry test vehicle[A].Toulouse, France,2001:14-23.
[24] Püttmann N.A Status report on RLV relevant flight experimentation in Germany[A].Toulouse, France,2001:7-12.
[25] Berge K D.German RLV activities[A].Huntsville, Alabama,2002:13-31.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%