期刊文献+

C/SiC复合材料在高能HAN发动机上应用研究 被引量:2

Research on application of C/SiC composite in high-energy HAN-based thruster
下载PDF
导出
摘要 针对高能硝酸羟胺(HAN)发动机特点,联合国防科技大学与贵研铂业股份有限公司研发了新型C/SiC复合材料身部,并进行地面试验。试验结果表明,C/SiC复合材料身部结构完好,表面HfO_2基环障涂层较完整,未出现显著开裂、剥落,涂层效果明显,保证了HAN单元发动机工作寿命。本研究为C/SiC身部在HAN单元发动机上工程化应用提供参考。 According to the characteristics of the high-energy Hydroxylammonium Nitrate (HAN) thruster, a novel carbon fiber reinforced silicon carbide composite (C/SiC) thruster chamber was developed and the ground hot fire test was carried out. The test result shows that the C/SiC com- posite chamber works well during the tests, the HfO2-based environmental barrier coating (EBC) on the chamber is intact, and there is no significant crack or spallation on it, which protects the com- posite against the corrosion of the combustion gases of the engine. This study provides a reference for the engineering application of C/SiC thruster chamber in HAN thruster.
出处 《火箭推进》 CAS 2017年第5期63-68,86,共7页 Journal of Rocket Propulsion
基金 国家863计划资助项目(2015AA7023023)
关键词 无毒单元推进剂 单组元发动机 C/SIC复合材料 环境障涂层 nontoxic monopropellant monopropellant engine C/SiC composite environmentalbarrier coating
  • 相关文献

参考文献2

二级参考文献8

  • 1[1]GORDON S, McBRIDE B J. Computer program for calculation of complex chemical equilibrium compositions, rocket performance, incident and reflected shocks, and chapman-jouguet detonations[R]. NASA SP-273, March 1976.
  • 2[2]NICKERSON G R, DANG L D, COATS D E. Two-dimensional kinetic performance computer program[R]. Software and Engineering Associates, Inc., Contract No. NAS8-35931, April 1985.
  • 3[3]DUNN S S, COATS D E. Nozzle performance predictions using the TDK97 Code[R], AIAA 97-2807.
  • 4BAKER C. A high temperature, light weight, nozzle materials, AIAA 94-2892 [R]. USA: AIAA, 1994.
  • 5STEFFIER W S, SHINAVSKI R J, RUSNAK C F, et al. Improved performance and durability of liquid propulsion rocket thrusters fabricated from triaxially braided C-SiC intraply hybrid-fiber/SiC matrix composites, ADA405477 [R]. USA: ADA, 2005.
  • 6MARTIN Minthorn. Advanced carbon fiber reinforced silicon carbide technology for SM3 divert and attitude control systems, N96-284[R]. [S.l.]: Fiber Material Inc., 2002.
  • 7SCHMIDT S, BEYER S, KNABE H, et al. Advanced ceramic matrix composites materials for current and future propulsion technology applications [J]. Acta Astronantica, 2004, 55 (3-9): 409-420.
  • 8邹武 张康助 张立同.陶瓷基复合材料在液体火箭发动机上的应用[J].固体火箭技术,2000,23:2-2.

共引文献8

同被引文献19

引证文献2

二级引证文献4

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部