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Proceedings Paper

Combustion-augmented laser ramjets
Author(s): Hideyuki Horisawa; Kazunobu Tamada; Itsuro Kimura
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Paper Abstract

A preliminary study of combustion-augmented laser-ramjets was conducted, in which chemical propellant such as a gaseous hydrogen/air mixture was utilized and detonated with a focused laser beam in order to obtain a higher impulse compared to the case only using lasers. CFD analysis of internal conical-nozzle flows and experimental measurements including impulse measurement were conducted to evaluate effects of chemical reaction on thrust performance improvement. From the results, a significant improvement in the thrust performances was confirmed with addition of a small amount of hydrogen to propellant air, or in combustion-augmented operation.

Paper Details

Date Published: 7 June 2006
PDF: 10 pages
Proc. SPIE 6261, High-Power Laser Ablation VI, 62612M (7 June 2006); doi: 10.1117/12.674646
Show Author Affiliations
Hideyuki Horisawa, Tokai Univ. (Japan)
Kazunobu Tamada, Tokai Univ. (Japan)
Itsuro Kimura, Univ. of Tokyo (Japan)


Published in SPIE Proceedings Vol. 6261:
High-Power Laser Ablation VI
Claude R. Phipps, Editor(s)

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