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等离子体屏蔽和稀疏波对冲量耦合系数的影响 被引量:5

Influences of plasma shielding and rarefaction wave on impulse coupling coefficient
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摘要 利用脉冲Nd:YAG激光作用在铝、铜靶上,研究了不同入射激光能量下冲量耦合系数和离焦量之间的关系,以及不同功率密度情况下冲量耦合系数和光斑直径的关系。实验表明铝靶在入射激光脉冲能量由75.8 mJ增加到382.3 mJ时,冲量耦合系数峰值对应的最佳离焦量由-10 mm处远离焦点向透镜方向移到-18 mm,而对应的激光功率密度仅由2.0×109W/cm2增加到3.9×109W/cm2;铜靶实验规律和铝靶类似。等离子体屏蔽的吸收作用导致了冲量耦合系数达到最大值后迅速降低。铝靶在入射激光功率密度由0.7×109W/cm2增大到1.0×1010W/cm2时,冲量耦合系数随光斑直径增大而增大,对应变化斜率由5.2×10-5N.s/(mm.J)增大到49.2×10-5N.s/(mm.J),表明了稀疏波对冲量耦合系数的削弱作用随入射激光功率密度增加而增加,随光斑直径增大而减小。 The relationship between the impulse coupling coefficient and the distance of the target from focus at different incident laser energy, and the relationship between impulse coupling coefficient and laser spot diameter at different incident laser intensity were studied by applying Nd.. YAG laser pulse on the AI(Cu) target. The experiments show that the target position corresponding to the peak impulse coupling coefficient moves towards to the lens with the increase of the laser energy, and the increase of the optimum intensity is small. These prove that the plasma shielding induces decreases impulse coupling coefficient to decrease after the peak value. On the other hand impulse coupling coefficient increases with the increase of the laser spot diameter in a linear way at the same incident laser intensity, and the slope is increased from 5.2×10^-5 N · s/(mm ·J) to 49.2×10^-5 N · s/(mm ·J) with the increase of the laser intensity from 0.7 GW/cm^2 to 10 GW/cm^2. This experimental result implies that the influence of the rarefaction wave on impulse coupling coefficient increases with the increase of the incident laser intensity, and decreases with the increase of the laser spot diameter.
出处 《强激光与粒子束》 EI CAS CSCD 北大核心 2007年第4期585-588,共4页 High Power Laser and Particle Beams
基金 国家自然科学基金资助课题(60578015)
关键词 等离子体屏蔽 稀疏波 冲量耦合系数 力学效应 Plasma shielding Rarefaction wave Impulse coupling coefficient Mechanical effect
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参考文献12

  • 1Phipps C R Jr,Turner T P,Harrison R F,et al.Impulse coupling to targets in vacuum by KrF,HF,and CO2 single-pulse lasers[J].J Appl Phys,1988,64(3):1083-1096.
  • 2Nehls M,Edwards D,Gray P.Ablative laser propulsion using multi-layered material systems[C]//Proc of 33^rd AIAA Plasmadynamics and Lasers Conference.2002:20-23.
  • 3Bass M,Nassar M A,Swimm R T.Impulse coupling to aluminum resulting from Nd:glass laser irradiation induced material removal[J].J Appl Phys,1987,61(3),1137-1144.
  • 4Pakhomov A V,Lin J,Kenneth A H.Effect of air pressure on propulsion with TEA CO2[C]//Proc of SPIE.2004,5448:1017-1027.
  • 5Kantrowitz A.Propulsion to orbit by ground-vased laser[J].Astronautics and Aeronantics,1972,10(5):74-76.
  • 6Phipps C R,Luke J R,Lippert T,et al.Micropropulsion using laser ablation[J].Appl Phys A,2004,79(4-6):1385-1389.
  • 7Schall W O,Bohn W L,Eckel H A.Lightcraft experiments in Germany[C]//Proc of SPIE.2000,4065:472-480.
  • 8Pakhomov A V,Lin L,Thompson M S.Specific impulse of ablative laser propulsion[C]//Proc of 42^nd AIAA Aerospace Science Meeting and Exhibit.2004:5-8.
  • 9童慧峰,唐志平,胡晓军,龚平,李静,蔡建,王声波,林丽耘.“烧蚀模式”激光推进的实验研究[J].强激光与粒子束,2004,16(11):1380-1384. 被引量:15
  • 10金星,洪延姬,崔村燕,王军,文明.激光推进冲量耦合系数的测量方法[J].强激光与粒子束,2004,16(7):861-864. 被引量:28

二级参考文献4

  • 1[1]Phipps C R, Reilly J P. Laser launching a 5kg object into low earth orbit[A]. Proc of SPIE[C]. 2000,4065: 502-510.
  • 2[2]Feikema D. Analysis of the laser propelled lightcraft vehicle[R]. AIAA-2000-2348.
  • 3[3]Myrabo L N, Messitt D G. Ground and flight tests of a laser propelled vehicle[R]. AIAA-1998-1001.
  • 4[4]Schall W O, Bohn W L, Echel H A. Light craft experiments in Germany[A]. Proc of SPIE[C]. 2000,4065: 472-480.

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