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Title: An Experimental and Conceptual Investigation of Laser Micro Propulsion

Journal Article · · AIP Conference Proceedings
DOI:https://doi.org/10.1063/1.2203268· OSTI ID:20800243
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  1. Laser Propulsion Laboratory, LMBD, Department of Modern Mechanics, University of Science and Technology of China, Hefei, 230026 (China)

The laser micro-impulse torsion pendulum has been developed in this lab. A thin glass plate of about 80{mu}m thick is made as the target holder where the propellant film sticks on. Such structure can be used for both the R-mode and the T-mode measurements. The minimal resolution of this apparatus is 3x10-9N.s. A package, which combines a 2W single LD with its lenses, is evaluated by the pendulum under R-mode and T-mode conditions, respectively, in this lab. the momentum coupling coefficient Cm is about 2dyn/W and the specific impulsion Isp is about 170s. A new conceptual fiber-distributed structure of laser micropropulsion system for microsatellites has been proposed and discussed in this article.

OSTI ID:
20800243
Journal Information:
AIP Conference Proceedings, Vol. 830, Issue 1; Conference: 4. international symposium on beamed energy propulsion, Nara (Japan), 15-18 Nov 2005; Other Information: DOI: 10.1063/1.2203268; (c) 2006 American Institute of Physics; Country of input: International Atomic Energy Agency (IAEA); ISSN 0094-243X
Country of Publication:
United States
Language:
English