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等离子体微推进技术的研究进展

叶继飞,洪延姬,王广宇,李南雷

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叶继飞, 洪延姬, 王广宇, 李南雷. 等离子体微推进技术的研究进展[J]. , 2011, 4(4): 319-326.
引用本文: 叶继飞, 洪延姬, 王广宇, 李南雷. 等离子体微推进技术的研究进展[J]. , 2011, 4(4): 319-326.
YE Ji-fei, HONG Yan-ji, WANG Guang-yu, LI Nan-lei. Research progress in micro-laser plasma propulsion[J]. Chinese Optics, 2011, 4(4): 319-326.
Citation: YE Ji-fei, HONG Yan-ji, WANG Guang-yu, LI Nan-lei. Research progress in micro-laser plasma propulsion[J].Chinese Optics, 2011, 4(4): 319-326.

等离子体微推进技术的研究进展

基金项目:

国家973重点基础研究发展规划资助项目(No.61328)

详细信息
    作者简介:

    叶继飞(1981-),男,吉林辽源人,硕士研究生,讲师,主要从事 微推进技术方面的研究。 E-mail:yjf1981@163.com

  • 中图分类号:TN249; V448.2

Research progress in micro-laser plasma propulsion

  • 摘要:为了加快 等离子体微推进技术(LPP)在航天领域的应用,介绍了该项技术近10年的发展状况。讨论了 等离子体微推进技术发展过程中衍生出的各种工作模式,并简略分析了不同工作模式的优缺点。着重介绍了靶特性对 微推进性能的影响,包括靶材的选择、靶的结构、靶材掺杂,以及靶物相特性等。针对该项技术的最终发展目标是研制微小卫星姿轨控的 等离子体微推力器( LPT),介绍并分析了美国Phipps小组开展的 微推力器的研制工作。最后,指出了 等离子体微推进技术目前存在的一些问题,并展望了它的发展前景。

  • [1] 王广宇,洪延姬,叶继飞. 微推进研究进展 . 中国宇航学会.2007年固体火箭推进第24届年会论文集 ,2007:367-372. WANG G Y,HONG Y J,YE J F. Research progress of the laser micro propulsion . Chinese Society of Astronautics. The 24th Solid Rocket Propulsion Symposium,2007:367-372.(in Chinese) [2] CLAUDE R P,MITAT B,WILLY B,et al.. Review:laser-ablation propulsion[J].J. Propulsion and Power,2010,26(4):609-637. [3] CLAUDE R P. Description of the photonic associates "LPT" thruster .Photonic Associates,LLC,2003:1-3. [4] PHIPPS C,LUKE J,ELGESON W. Laser space propulsion overview[J]. SPIE,2007,6606:660602. [5] 唐志平. 烧蚀模式 推进的机理和应用探索[J]. 中国科学技术大学学报 ,2007,37(10):1300-1306. TANG ZH P. Exploration of mechanism and applications for ablation laser propulsion[J].J. University Sci. Technol. China,2007,37(10):1300-1306.(in Chinese) [6] 张翼,郑志远,鲁欣,等. 等离子体微推进技术研究进展[J]. 科技导报 ,2007,25(19):70-74. ZHANG Y,ZHENG ZH Y,LU X,et al.. Development of laser plasma micro-propulsion[J].Science and Technology.,2007,25(19):70-74.(in Chinese) [7] 叶继飞,洪延姬,王广宇. 微推进的靶特性研究进展[J]. 推进技术 ,2009,30(6):751-756. YE J F,HONG Y J,WANG G Y. Progress of research in laser micro ablation of target[J].J. Propulsion Technol.,2009,30(6):751-756.(in Chinese) [8] JAMES R L,CLAUDE R P,GLEN G M. Laser plasma thruster continuous thrust experiment[J].SPIE,2002,4760:843-851. [9] CLAUDE R P,JAMES R L,THOMAS L,et al.. Micropropulsion using a laser ablation jet[J].J. Propulsion Power,2004,20(6):1000-1011. [10] CLAUDE R P,JAMES R L. Advantages of a ns-pulse micro-laser plasma thruster[J]. AIP Conf. Proc.,2003,664:230-239. [11] SOOJIN C,TAEHEE H,ARDIAN B G,et al.. Thrust enhancement via gel-type liquid confinement of laser ablation of solid metal propellant[J].Appl. Phys. A,2010,98:147-151. [12] 洪延姬,王广宇,窦志国. 烧蚀微推力器研究进展[J]. 航空学报 ,2009,30(9):1555-1565. HONG Y J,WANG G Y,DOU ZH G. State of art of laser ablation mierothruster[J].Acta Aeronautica Et Astronautlca Sinica,2009,30(9):1555-1565.(in Chinese) [13] ANDREW V,PAKHOMOV M,SHANE T,et al.. Ablative laser propulsion:a study of specific impulse, thrust and efficiency[J]. AIP Conf. Proc.,2003,664:194-205. [14] CLAUDE R P,JAMES R L,WESLEY H,et al.. 3ks specific impulse with a ns-pulse laser microthruster . International Electric Propulsion Conference,Princeton,NJ,Oct 30-Nov 4,2005:319-322. [15] CLAUDE R P.Laser Ablation and Its Applications[M]. Berlin:Springer-Verlag,2007. [16] SCHALL W O,ECHEL H-A,TEGEL J,et al.. Characterization of the absorption wave produced by CO2laser ablation of a solid propellant,FA8655-04-1-3067 .Stuffgart:German Aerospace Center Institute of Technical Physics,2005. [17] MASAKATSU N,HIROYUKI K,TAKAYOSHI I,et al.. Experimental investigation of a chemically-augmented, diode laser thruster for micro spacecraft[J].AIAA,2004:2004-3799. [18] 蔡建. 微推进的原理和应用研究 . 合肥:中国科技大学 ,2007. CAI J. Mechanism and experiment investigation of laser micro-propulsion . Hefei:University of Seience&Technology of China,2007.(in Chinese) [19] ANDREW V P,JOHN E S. A conceptual tree of laser propulsion[J].AIP Conf. Proc.,2008,997:592-603. [20] FABBRO R,FOURNIER J,BALLARD P,et al.. Physical study of laser-produced plasma in confined geometry[J].J. Appl. Phys.,1990,68:775-784. [21] SHIGEAKI U,KAZUHISA H,KAZUHISA F,et al.. Comparison of surface and internal laser irradiation of solid propellant for propulsion[J].AIAA,2002:2002-2155. [22] SHIGEAKI U,KAZUHISA H,KAZUHISA F,et al.. Characteristics of volume expansion of laser plasma for efficient propulsion[J].SPIE,2002,4760:810-820. [23] CLAUDE R P,DANIEL B S,ROBERT R,et al.. Very high coupling coefficients at low laser fluence with a structured target[J].SPIE,2000,4065:931-938. [24] 程建中,蔡建,胡云,等. 掺杂金属颗粒的高分子工质 推进实验研究[J]. 强 与粒子束 ,2008,20(7):1190-1194. CHENG J ZH,CAI J,HU Y,et al.. Experimental study of laser propulsion by using polymer propellant doped with metal powder[J].High Power Laser and Particle Beams,2008,20(7):1190-1194.(in Chinese) [25] LIPPER T T,DAVID C,HAUER M,et al.. Tailor-made polymers for laser ablation[J].Review of Paser Engineering,2001,29(11):734-738. [26] SHIGEAKI U. Efficient laser ablation,AOARD 044033 . Tokyo:Tokyo Institute of Technology,2006. [27] ROMAIN F,LUKAS U,THOMAS L,et al.. Laser ablation of energetic polymer solutions:effect of viscosity and fluence on the splashing behavior[J].Appl. Phys. A,2008,47:78-87. [28] LIPPERT T,URECH L,FARDEL R,et al.. Materials for laser propulsion:"liquid" polymers[J].SPIE,2008,7005:750012. [29] CLAUDE R P,JAMES R L,THOMAS L,et al.. Liquid-fueled, laser-powered, N-class thrust space engine with variable specific impulse[J].AIP Conf. Proc.,2008:222-231.
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出版历程
  • 收稿日期:2011-05-12
  • 修回日期:2011-07-23
  • 刊出日期:2011-08-25

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