陶瓷纤维刚性隔热瓦具有轻质、耐高温和低热导率等优点,是目前美国航天飞机最主要的热防护材料之一.介绍了陶瓷纤维刚性隔热瓦的制备方法,详细叙述了美国三代刚性隔热瓦在制备工艺和性能方面的研究进 展,总结了国内刚性隔热瓦的研究现状,并展望了刚性隔热瓦的发展趋势.
参考文献
| [1] | 张志成.高超声速气动热和热防护[M].北京:国防工业出版社,2003 |
| [2] | Komine A;Kobayashi A S .Interfacial fracture of spaceshuttle thermal-protection system[J].Experimental Mechanics,1982,22(12):454. |
| [3] | 王衍飞 .气凝胶复合陶瓷纤维刚性隔热瓦的制备及性能研究[D].国防科学技术大学,2008. |
| [4] | 王思青,张长瑞,周新贵,程海峰,冯坚,曹英斌.重复使用运载器陶瓷热防护系统[J].导弹与航天运载技术,2004(03):37-41. |
| [5] | 关春龙,李垚,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(06):7-11,42. |
| [6] | 苏芳,孟宪红.三种典型热防护系统发展概况[J].飞航导弹,2006(10):57-60. |
| [7] | 曾昭焕 .航天飞机用刚性陶瓷瓦防热材料发展概况[J].宇航材料工艺,1989,19(03):12. |
| [8] | Bealey R M;Izu Y D;Nakano H N.Fabrication and improvement of LMSC's all-silica RSI[J].Techn Report NASA TMX-2719,1973(01):1. |
| [9] | Banas R P;Gzowski E R;Larson W L .Processing aspects of the space shuttle orbiter's ceramic reusable surface insulation[J].Ceramic Engineering and Science Proceedings,1983,4(7-8):591. |
| [10] | Fletcher J C;Goldstein H E;Smith M et al.Silica reusable surface insulation[P].US,3952083,1976-04-20. |
| [11] | Parmenter KE.;Shuman K.;Milstein F.;Szalai CE.;Tran HK.;Rasky DJ. .Compressive response of lightweight ceramic ablators: Silicone impregnated reusable ceramic ablator[J].Journal of spacecraft and rockets,2002(2):290-298. |
| [12] | Frosch R A;Leiser D B;Goldstein H E et al.Fibrous refractory composite insulation[P].US,4148962,1979-04-10. |
| [13] | Green D .Fracture toughness/young's modulus correlation for low-density fibrous silica bodies[J].Journal of A C S G,1983,65(04):288. |
| [14] | Schramm W .HRSI and LRSI-the early year[J].Ceramic Bulletin,1981,60(11):12. |
| [15] | Leiser D B;Smith M et al.Options for improving rigidized ceramic heatshields[J].Ceramic Engineering and Science Proceedings,1985,6:757. |
| [16] | Leiser D B;Smith M;Stewart D A .Effect of fiber size and composition on mechanical and thermal properties of low density ceramic composite insulation materials[J].NASA CP,1984,2357:231. |
| [17] | DiChiara R A .Method of making a permeable ceramic tile insulation[P].US,6613255,2003-09-02. |
| [18] | Stewart D A;Leiser D B;Smith M.Thermal response of integral multicomponent composite thermal protection systems[AIAA-85-1056][A].,1985 |
| [19] | Hinkle K A;Staszak P R;Watts E T.Advanced ceramic materials development and testing[AIAA-96-1527][A].,1996:525. |
| [20] | Banas R P;Creedon J F;Cunnington J R.Thermophysical and mechanical properties of the HTP family of rigid ceramic insulation materials[ AIAA-85-1055][A].,1985 |
| [21] | Heng V;Hinkle K A;Santos M A .Rigid insulation and method of producing same[P].US,6716782,2004. |
| [22] | Chiu S A;Pitts W C.Reusable surface insulations for reentry spacecraft, AIAA-91-0695[A].,1991 |
| [23] | Leiser D B;Smith M;Stewart D A.Thermal and mechanical properties of advanced high temperature ceramiccomposite insulation[J].Ceramic Engineering and Science Proceedings,1983(04):551. |
| [24] | Stewart D A;Leiser D B.Thermal stability of ceramic coated thermal protection materials in a simulated high-speed earth entry[J].Ceramic Engineering and Science Proceedings,1988(09):1199. |
| [25] | 王钦,胡子君,孙陈诚,鲁胜,李俊宁.陶瓷隔热瓦力学性能影响因素及其稳定性控制[J].宇航材料工艺,2010(02):77-79. |
| [26] | 孙陈诚,胡子君,鲁胜,张宏波,陈海坤.刚性隔热材料的力学性能[J].宇航材料工艺,2010(02):74-76. |
| [27] | 朱庆霞,梁华银,丁志坚.莫来石纤维多孔陶瓷的制备与性能[J].中国陶瓷,2006(10):7-9. |
| [28] | 高庆福 .纳米多孔SiO<,2>、Al<,2>O<,3>气凝胶及其高效隔热复合材料研究[D].国防科学技术大学,2009. |
| [29] | 王衍飞,张长瑞,冯坚,姜勇刚.SiO2气凝胶复合短切莫来石纤维多孔骨架复合材料的制备及性能[J].国防科技大学学报,2008(06):24-28. |
| [30] | Amanda S;William C.Reusable surface insulation for reentry spacecraft[AIAA-91-0695][A].,1991 |
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：
-
10%
-
20%
-
30%
-
40%
-
50%