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激光微烧蚀固体靶材羽流流场演化特性 被引量:7

Plume field evolvement characteristics of the laser micro ablation for solid target
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摘要 激光微推进技术是激光推进技术的重要分支,其主要用于研制一种用于卫星姿轨控的激光微推力器。激光微烧蚀靶材形成的羽流流场演化特性及其所表征的力学性能是激光微推进技术研究的热点问题。针对激光微烧蚀靶材所形成羽流流场的特点,采用纹影光学显示方法,实现了毫米尺度的带有自发光的激光烧蚀固体靶材微秒时间尺度的羽流流场观测。选取典型的聚合物材料作为靶材,分析了激光微烧蚀聚合物靶材的羽流演化特性,并对不同靶材获得的流场演化特征进行对比,结果表明:PVC材料更适合于作为激光微推进固体工质的选材。 The laser micro propulsion is one of the important branch of laser propulsion research field. The laser micro thruster is typically used for the satellite gesture and orbit control. The plume field evolvement and the thrust formation characteristics of laser micro ablation are hot research points. According to the characteristics of the plume field evolvement, take the schlieren technology as the flow visualization method, a millimeter scale distinct, with self- luminescence, and microsecond time freezing data image could be obtained. Nine kinds of solid poly- mers were taken as the targets, the process of the plume field evolvement was contrasted and analyzed, the result shows that, the PVC is the best solid target choice for the laser micro propulsion
出处 《红外与激光工程》 EI CSCD 北大核心 2013年第S01期47-51,共5页 Infrared and Laser Engineering
基金 国家自然科学基金(11102234)
关键词 激光推进 工质 纹影 流动显示 laser propulsion propellant schlieren flow visualization
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  • 1刘向阳,范宁军,李科杰.微型推进器推力测试的现状及发展趋势[J].测控技术,2004,23(5):18-20. 被引量:23
  • 2冯天植.彩色纹影技术在复杂流场显示中的应用[J].华东工学院学报,1993(1):80-83. 被引量:1
  • 3张惠明,赵奎翰,息树和,魏建勤,刘文胜,周作恒.直喷式柴油机燃烧室形状对碳粒形成过程影响的试验研究[J].内燃机学报,1996,14(3):286-294. 被引量:8
  • 4王广宇,金星,叶继飞.激光干涉仪测微冲量原理[J].推进技术,2007,28(5):530-533. 被引量:6
  • 5Bonnal C, Ruault J, Desjean M. Active debris removal: Recent progress and current trends [J]. Acta Astronautica, 2013, 85: 51-60.
  • 6Kaplan M H. Survey of Space Debris Reduction Methods[R]. AIAA-2009-6619, 2009.
  • 7Bruno Esmiller, Christophe Jacquelard, Hans-Albert Eckel, et al. Space debris removal by ground-based lasers: main conclusion of the European project CLEANSPACE [J]. Applied Optics, 2014, 53(31): 45-54.
  • 8James T Early, Camille Bibeau, Claude Phipps. Space debris de-orbiting by vaporization impulse using short pulse laser [C]// High-Power Laser Ablation V, Proceedings of SPIE, 2004, 5448(PART1): 441-449.
  • 9Remi Soulard, Mark N Quinn, Toshiki Tajima, et al. ICAN: a novel laser architecture for space debris removal [J]. Acta Astronautiea, 2014, 105: 192-200.
  • 10P hipps C R. A laser optical system to re-enter or lower low earth orbit space debris[J]. Acta Astronautiea, 2014, 93: 20-33.

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