期刊文献+

自由分子流微电热推力器流动模拟与性能预示

Flow Simulation and Performance Prediction of Free Molecule Micro-resistojet
下载PDF
导出
摘要 为了精确的预示自由分子流推力器(FMMR)在不同工质、工况下的性能,采用直接模拟蒙特卡罗(DSMC)方法模拟FMMR内气体流动,计算了不同工质气体、工作压强和加热温度条件下的FMMR推力、比冲等性能,分析了工质、工作压强和加热温度对FMMR性能的影响。计算和分析结果表明,工质气体的选择不影响FMMR的推力性能,但随着工质气体相对分子质量的减小,推力器比冲迅速增加;在总压50~500Pa,温度300~600K条件下,推力器的比冲随总压和加热温度的增大而增加,推力随加热温度增大而减小,随总压增大而增大。 To accurately predict the performance of FMMR, under different propellant and working conditions, Direct simulation Monte Carlo method was used to simulate the gas flow in FMMR. The thrust and specific impulse of FMMR were calculated, and the influence of propellant types, working pressure as well as heating temperature on the performance of FMMR was studied. Results of calculation and analysis show that the propellant kind has no effect on thrust, while specific impulse rapidly increases with the decreasing of propellant molecule weight; the specific impulse of FMMR increases with the height of working pressure and heating temperature, and thrust increases with the increasing of the working pressure but decreases with the increasing of the heating temperature.
出处 《中国空间科学技术》 EI CSCD 北大核心 2008年第2期66-71,共6页 Chinese Space Science and Technology
基金 武器装备预研基金项目(9140C52030106HK0)
关键词 微推进 自由分子流推力器 直接模拟蒙特卡罗法 数值模拟 航天器 Micro-propulsion Numerical simulation Spacecraft Free molecule micro-resistojet Direct Simulation Monte Carlo
  • 相关文献

参考文献8

  • 1AHMED Z, GIMELSHEIN S F, KETSDEVER A. Numerical analysis of free-molecule micro-resistojet performance[J]. Journal of Propulsion and Power, 2006, 22(4): 749-756.
  • 2KETSDEVER A, GREEN A, MUNTZ E P, et al. Fabrication and Testing of Free Molecule Micro-resistojet: Initial Result[R]. AIAA 2000-3672. July, 2000.
  • 3KETSDEVER A, WADSWORTH D. The free molecule micro-resistojet., an interesting alternative to nozzle expansion[R]. AIAA 98-3918. July, 1998.
  • 4韩先伟,唐周强,陶文铨,张贵田,张恩昭.自由分子流微电热推力器数值模拟计算[J].固体火箭技术,2004,27(3):184-189. 被引量:3
  • 5韩先伟,唐周强,陶文铨,张贵田,张恩昭.自由分子流微电热推力器工作特性和性能研究[J].固体火箭技术,2005,28(2):83-86. 被引量:4
  • 6韩先伟,周军,唐周强,郭斌,张恩昭.微型推进系统技术方案研究[J].火箭推进,2005,31(1):1-7. 被引量:6
  • 7KAMIADAKIS G E, BESKOK A. Micro Flows Fundamentals and Simulation[M]. Springer-Verlag New York, 2002.
  • 8BIRD G A. Molecular Gas Dynamics and Direct Simulation of Gas Flow[M]. Clarendon, Oxford, 1994.

二级参考文献17

  • 1韩先伟,唐周强,陶文铨,张贵田,张恩昭.自由分子流微电热推力器数值模拟计算[J].固体火箭技术,2004,27(3):184-189. 被引量:3
  • 2[1]Michael M Micci, Andrew D, Ketsdever.Micro- propulsion for Small Spacecraft [M].American Institute of Aeronautics and Astronautics Inc.
  • 3[3]Amanda A Green.Demonstration and Quantitative Characterization of a MEMS Fabricated Propulsion System for the Next Generation of Microspacraft [R].AIAA 2001-0009.
  • 4[4]Xiong Jijun, Zhou Zhaoying, Ye Xiongying, et al.Measurement μN Thrust for the Micro Colloid Thruster [C].Proceedings of 5th International Symposium on Test and Measurement,2003.
  • 5[6]Wong J, Ketsdever A, Reed H.Numerical Modeling of the Free Molecule Micro-Resistojet Prototype and Next Generation Designs Evaluation [R].AIAA 2003-3581.
  • 6[7]Reni, Raju, Subrata Roy.Modeling Single Component Fluid Transport through Micro Channels and Free Molecule Micro-Resistojet [R].AIAA 2004-1342.
  • 7Micci Michael M, Ketsdever Andrew D. Micropropulsion for small spacecraft [M].Progress in Astronautics and Aeronautics, American Institue of Aeronautics and Astronautics, Inc., Vol.187.
  • 8Green Amanda A. Demonstration and quantitative characterization of a MEMS fabricated propulsion system for the next generation of microspacraft[R]. AIAA 2001-0009.
  • 9Hammel Jeffrey Robert. Development of an unstructured 3-D direct simulation monte carlo/particle-in-cell code and the simulation of microthruster flows [R].Degree of Master in worcester polytechnic institute, 2002, 8.
  • 10Wong J, Ketsdever A, Reed H. Numerical modeling of the free molecule micro-resistojet prototype and next generation designs evaluation[R].AIAA 2003-3581.

共引文献9

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