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Z. Zheng, J. Zhang, Y. Zhang, F. Liu, M. Chen, X. Lu, Y. Li (2006)
Enhancement of coupling coefficient of laser plasma propulsion by water confinementApplied Physics A, 85
T. Yabe, Hirokazu Ohzono, T. Ohkubo, Choijil Baasandash, M. Yamaguchi, T. Oku, Kazumoto Taniguchi, S. Miyazaki, R. Akoh, Y. Ogata, B. Rosenberg, M. Yoshida (2004)
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Experimental Study of the Momentum Coupling Coefficient with the Pulse Frequency and Ambient Pressure for Air‐Breathing Laser Propulsion, 830
C. Favre, V. Boutou, S. Hill, W. Zimmer, M. Krenz, H. Lambrecht, Jin Yu, R. Chang, L. Woeste, J. Wolf (2002)
White-light nanosource with directional emission.Physical review letters, 89 3
L. Urech, T. Lippert, C. Phipps, A. Wokaun (2007)
Polymer ablation: From fundamentals of polymer design to laser plasma thrusterApplied Surface Science, 253
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Micropropulsion Using a Laser Ablation JetJournal of Propulsion and Power, 20
T. Yabe, C. Phipps, K. Aoki, M. Yamaguchi, Ryou Nakagawa, Choijil Baasandash, Y. Ogata, M. Shiho, Gen Inoue, M. Onda, K. Horioka, I. Kajiwara, K. Yoshida (2003)
Laser-driven vehicles – from inner-space to outer-spaceApplied Physics A, 77
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Extended measurement of crater depths for aluminum and copper at high irradiances by nanosecond visible laser pulsesApplied Surface Science, 255
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Kyung-Cheol Lee, Kihong Kim, J. Yoh (2008)
Modeling of high energy laser ignition of energetic materialsJournal of Applied Physics, 103
J. Yoh, Hyunhee Lee, Jihun Choi, Kyung-Cheol Lee, Kihong Kim (2008)
Ablation-induced explosion of metal using a high-power Nd:YAG laserJournal of Applied Physics, 103
Y. Zhang, X. Lu, Z. Zheng, F. Liu, P. Zhu, H. Li, Y. Li, Y. Li, J. Zhang (2008)
Transmitted laser propulsion in confined geometry using liquid propellantApplied Physics A, 91
T. Ohkubo, T. Yabe, S. Miyazaki, Choijil Baasandash, Kazumoto Taniguchi, Akito Mabuchi, Daisuke Tomita, Y. Ogata, Jun Hasegawa, Kazuhiro Horioka (2005)
Laser Propulsion Using Metal‐Free Water Cannon Target, 766
Laser propulsion has been developed as a suitable small thruster technology for the attitude control of micro and nano class satellites. Laser-based thrusters meet the satellite design criteria for being of light weight and cost effective, because they do not require fuel storing and oxidizer for combustion. Also, thrust control by laser propulsion is achieved fairly easy. In this paper, we consider the confinement of plasma expansion by a gel-type liquid material, which results in the enhancement of the thrust for propulsion. We also present our attempts to resolve some known issues regarding laser ablation of solid and liquid targets. The level of thrust is quantified via the momentum coupling coefficient, which was experimentally measured using a ballistic pendulum system. We have discovered that the laser ablation confinement by the gel-type medium results in 2.3 times more enhanced driving force as compared to the water confinement. A proof of performance is demonstrated for using gel-type material for generating propulsion, and material characterization for optimal thrust performance is presented.
Applied Physics A: Materials Science Processing – Springer Journals
Published: Oct 10, 2009
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