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概述化学气相沉积技术的一般原理与技术,总结化学气相沉积技术在材料制备方面的发展与应用状况,着重介绍化学气相沉积技术在制备贵金属薄膜和涂层领域的最新进展.

参考文献

[1] 孟广耀.化学气相淀积与无机新材料[M].北京:科学出版社,1984
[2] 王亚新;Angus J C.材料科学技术进展与展望[M].北京:中国科学技术出版社,1995
[3] 羽卒 .[J].高技术新材料快报,1997,7:1.
[4] 钟俊辉 .[J].稀有金属材料与工程,1993,22(04):82.
[5] Vargas J R;Goto T;Zhang W .[J].Applied Physics Letters,1994,65(09):1094.
[6] GotoT;Vargas J R;Hirai T.[J].Materials Science and Engineering,1996:223.
[7] GotoT;Vargas J R;Hirai T .[J].Journal of De Physique IV,1993,3:297.
[8] Gerfin T;Halg W J;Atamny F .[J].Thin Solid Films,1993,241:352.
[9] Kwak B S;First P N;Erbil A .[J].Journal of Applied Physics,1992,72(08):3735.
[10] XUE Z;Strouse M J;Shuh D K .[J].Journal of the American Chemical Society,1989,111:8779.
[11] Koplitz L V;Shuh D K;Chen Y J .[J].Applied Physics Letters,1988,53(18):1705.
[12] Ramke W G .High Temperature Protective Coatings for Graphite[R].Technical Report ML-TDR-64-173,1964.
[13] Macklin B A;Lamar P A .Development of Improved Methods of Depositing Iridium Coatings on Graphite[R].AD843766,1968.
[14] Harding J T;Kazaroff J M;Appel M A.Proceedings of the Second International Conference on Surface Modification Technologies[C].Chicago,1988:10.
[15] Wooten J R;Lawsaw P T .High-temperature,Oxidation-Resistant Thruster Research[P].NASA CR-185233,1990.
[16] Jassowski D M .Advanced Small Rocket Chambers Basic Program and Option Ⅱ-fundamental Processes and Material Evaluation[P].NASA CR-195349,1993.
[17] Jassowski D M;Schoenman L .Advanced Small Rocket Chambers Basic Program and Option 3-110 1bf Ir-Re Rocket Volume Ⅰ[P].NASA CR-195435,1995.
[18] Schneider S J .High-temperature Thruster Technology for Spacecraft Propulsion IAF-91-54[Z].,1991.
[19] 胡昌义;邓德国;高逸群 .[J].宇航材料工艺,1998,28(03):7.
[20] 黎鼎鑫;张永俐;袁弘鸣.贵金属材料学[M].长沙:中南工业大学出版社,1991:435.
[21] Tung Y L;Tseng W G;Lee C Y .[J].Organometallics,1999,18(05):864.
[22] Hierso J C;Satto C;Feurer R .[J].Chemistry of Materials,1996,8(10):2481.
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