概述了国内外姿/轨控液体火箭发动机高温抗氧化涂层的研究和应用进展,研制过程涉及多种材料体系,但仅有几类广泛应用于型号,包括Nb基材表面硅化物材料体系、Pt-Rh合金、Re基材表面Ir涂层.随着对发动机性能要求的提高,Re/Ir材料体系成为目前主要的研究方向.
参考文献
| [1] | 萨顿GP;比布拉兹O;洪鑫.火箭发动机基础[M].北京:科学出版社,2003:143. |
| [2] | 刘昌国,张中光,韩宏印,汪允武,孙得川.高比冲双组元液体远地点火箭发动机研究[J].上海航天,2003(04):30-33. |
| [3] | 美国国家材料咨询委员会所属涂层委员会.高温抗氧化涂层[M].北京:科学出版社,1980:16. |
| [4] | Wood R S .Experiences with high temperature materials for small thrusters[AIAA93-1962][R].,1993. |
| [5] | Ong J N;Fassell W M.Kinetics of oxidation of columbium and other refractory metals[J].Corrosion,1962(18):3821-3829. |
| [6] | Dotson L E .LB-2 processing of mcdonnell F-48 finrulder components[DMIC Report 167][R].,1962. |
| [7] | Wurst;Cherry .The evaluation of materials systems for high temperature aerospace application[AFML-TR-67-165][R].,1967. |
| [8] | Fitzgerald B G;Gezer N M .The reuse of fused slurry silicide coated Nb[AIAA70-279][R].,1970. |
| [9] | Friffiths V .A metallographic evaluation of some coated columbium alloys[NASA-CR-127 917][R].,1972. |
| [10] | Conrardy W P;Blumentthal H .Development of powder and gas cementation process for coating molybdenum alloys for high temperature protection[AD603021][R].,1964. |
| [11] | Moreton R .The Protection of tantalum form oxidation at high temperature with aluminium-50% Ti coatings[AD-634909][R].,1980. |
| [12] | Lawthers D D .Development of coatings for protection of high strength tantalum alloys in severs high temperature enviorments[AD-830322][R].,1985. |
| [13] | Gotzig U;Schulte G;Sows A .New generation 10N bipropellant MMH/NTO Thruster with double seat valve[AlAA 99-2594][R].,1999. |
| [14] | Carl Stechman;Peter WolI .A high performance liquid rocket engine for satellite main propulsion[AIAA 2000-3161][R].,2000. |
| [15] | Fearn J D G;Fiddick M J;Gould R D .Space propulsion research and development in the UK[AIAA 91-1938][R].,1991. |
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