7 June 2006 Combustion-augmented laser ramjets
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Proceedings Volume 6261, High-Power Laser Ablation VI; 62612M (2006) https://doi.org/10.1117/12.674646
Event: High-Power Laser Ablation 2006, 2006, Taos, NM, United States
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.
© (2006) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Hideyuki Horisawa, Hideyuki Horisawa, Kazunobu Tamada, Kazunobu Tamada, Itsuro Kimura, Itsuro Kimura, "Combustion-augmented laser ramjets", Proc. SPIE 6261, High-Power Laser Ablation VI, 62612M (7 June 2006); doi: 10.1117/12.674646; https://doi.org/10.1117/12.674646
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