Volume 44 Issue 1
Feb.  2015
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Ye Jifei, Hong Yanji, Li Nanlei. Impulse coupling performance of liquid propellant with ns laser micro ablation[J]. Infrared and Laser Engineering, 2015, 44(1): 102-106.
Citation: Ye Jifei, Hong Yanji, Li Nanlei. Impulse coupling performance of liquid propellant with ns laser micro ablation[J]. Infrared and Laser Engineering, 2015, 44(1): 102-106.

Impulse coupling performance of liquid propellant with ns laser micro ablation

  • Received Date: 2014-05-11
  • Rev Recd Date: 2014-06-13
  • Publish Date: 2015-01-25
  • Laser micro-propulsion is a new laser-powered electric propulsion technology, which uses the mechanical effect generated by laser-matter interaction. Liquid as propellant is the latest points of interest. Impulse coupling characteristics of interaction between liquid and laser decided the merits of propulsive performance. Torsion pendulum device was used to measure the micro-impulse. Monopropellant gel propellant, GAP and glycerol were used as propellant. Impulse and impulse coupling coefficient were measured under different laser energy. GAP obtained higher impulse coupling coefficient and was further studied. The results show that impulse coupling characteristics of GAP are better. Impulse coupling coefficient is generally greater than 500 uN/W, maximum is 1 493.0 uN/W. However, specific impulse and ablation efficiency are relatively low. Maximum specific impulse is 140 s; maximum ablation efficiency is 37.6%.
  • [1] Zhang Nan, Xu Zhijun, Zhu Xiaonong, et al. Laser propulsion technology [J]. Infrared and Laser Engineering, 2011, 40 (6): 1025-1037. (in Chinese)
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    [3] Shigeaki U, Masafumi B. Characterization of liquid propellant for improved LOTV mission[C]//Beamed Energy Propulsion: First International Symposium on Beamed Energy Propulsion, 2003: 214-222.
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    [5] Fardel R, Urech L, Lippert T, et al. Laser ablation of energetic polymer solutions: effect of viscosity and fluence on the splashing behavior [J]. Appl Phys A, 2009, 94: 657-665.
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    [7] Phipps C R, James R L. Liquid-fueled, laser-powered, Nclass thrust space engine with variable specific impulse [C]// Beamed Energy Propulsion, Fifth International Symposium, 2008: 222-231.
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    [10] Ye Jifei, Hong Yanji. Laser interference differential measurement of micro impulse based on the torsion balance[J]. Journal of Applied Optics, 2013, 34 (6): 990-994. (in Chinese)
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    [12] Lippert T, Hauer M, Phipps C R, et al. Fundamentals and applications of polymers designed for laser ablation [J]. Appl Phys A, 2003, 77: 259-264.
    [13] Zhao Yan, Xie Hongtao, Yuan Wei, et al. Research on preparation and properties of gel propellant DT-3 [J]. Chemical Propellants Polymeric Materials, 2010, 8 (2): 49-51. (in Chinese)
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    [15] Phipps C R, Birkan M, Bohn W, et al. Review: laser-ablation propulsion [J]. Journal of Propulsion and Power, 2010, 26(4): 609-637.
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    [18] Phipps C R, Luke J R, Lippert T, et al. Micropropulsion using a laser ablation jet [J]. Journal of Propulsion and Power, 2004, 20(6): 1000-1011.
    [19] Lippert T, David C, Hauer M, et al. Novel applications for laser ablation of photoploymers[J]. Applied Surface Science, 2002, 186: 14-23.
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Impulse coupling performance of liquid propellant with ns laser micro ablation

  • 1. State Key Laboratory of Laser Propulsion & Application,Academy of Equipment,Beijing 101416,China

Abstract: Laser micro-propulsion is a new laser-powered electric propulsion technology, which uses the mechanical effect generated by laser-matter interaction. Liquid as propellant is the latest points of interest. Impulse coupling characteristics of interaction between liquid and laser decided the merits of propulsive performance. Torsion pendulum device was used to measure the micro-impulse. Monopropellant gel propellant, GAP and glycerol were used as propellant. Impulse and impulse coupling coefficient were measured under different laser energy. GAP obtained higher impulse coupling coefficient and was further studied. The results show that impulse coupling characteristics of GAP are better. Impulse coupling coefficient is generally greater than 500 uN/W, maximum is 1 493.0 uN/W. However, specific impulse and ablation efficiency are relatively low. Maximum specific impulse is 140 s; maximum ablation efficiency is 37.6%.

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