期刊文献+

低功率氮气电弧加热推力器稳定性的实验研究 被引量:1

Experimental Study on Stability of Low Power Nitrogen Arcjet
下载PDF
导出
摘要 电弧加热推力器的稳定性是关系到推力器可靠性和寿命的关键问题。在分析影响稳定性的各种因素基础上,对传统低功率氮气电弧加热推力器进行性能测试,并总结了影响推力器稳定工作参数的原因,通过改进推力器的阳极结构,人为地将阳极弧点位置约束在扩张段,在工作稳定性和烧蚀方面获得了明显改善。 The stability of arcjet is the key relating to reliability and lifetime of thruster.On basis of analyzing the factor influencing on the stability of arcjet,the performance and stability rule for conventional low power nitrogen arcjet were acquired.According to reason of effect on stability,changes were made toward the anode structure,which pushes the arc anode attachment to the divergent section of the nozzle.The stability and ablation of new arcjet are improved.
出处 《宇航学报》 EI CAS CSCD 北大核心 2007年第6期1664-1667,共4页 Journal of Astronautics
基金 国家自然科学基金资助(60574031)
关键词 低功率 电弧加热推力器 稳定性 Low power Arcjet Stability
  • 相关文献

参考文献3

  • 1[1]Nakanishi S.Experimental performance of a 1-kilowatt arcjet thruster[R].NASA Technical Memorandum 87131,1985
  • 2[2]Saccoccia G.Electric propulsion in ESA[C].40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,Fort Lauderdale,Florida,2004,AIAA-2004-3329
  • 3[6]Lichon P G.Development and demonstration of a 600-second mission-average Isp arcjet[J].Journal of Propulsion and Power,1996,12(6):1018-1025

同被引文献7

  • 1汤海滨,刘畅,陈树君,马彬,刘宇.电弧加热发动机地面试验(Ⅱ)发动机电特性分析[J].推进技术,2006,27(6):546-549. 被引量:5
  • 2AUWERWE K M, GLOCKER B, GOELZ T, et al. Arcjet thruster development[J]. Journal of Propulsion and Powers, 1996, 12(6): 1077-1083.
  • 3ALTENBURGER G P, KING R J. Simulation the arcjet thruster using a nonlinear active load. AIAA-92-3528 [ R]. Indianapolis: AIAA Press, 1992.
  • 4RONALD A S, JEFFREY A P, JOHN H S, et al. Performance effects of interaction between a low-power Arcjet and its power processing unit. AIAA-92-3238[R]. Nashville: AIAA Press, 1992.
  • 5MCLEAN C H, LICHON P G, SANKOVIC J. Life demonstration of a 600-second mission average Arcjet, AIAA-94-2866 [R]. Indianapolis: AIAA Press, 1994.
  • 6BUTLER G W, CASSADY R J. Directions for arcjet technology development[J]. Journal of Propulsion and Powers, 1996, 12(6) : 1026-1034.
  • 7LAMBERT K M, ZAMAN A J, CURRAN F M. Experimental demonstration of the effects of an electric thruster plasma plume on microwave propagation[J]. Antennas and Propagation Society International Symposium, 1995(4): 1734-1737.

引证文献1

二级引证文献1

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