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- W2332920001 abstract "Ducted rockets are one kind of ramjet engines which are air-breathing propulsion system suited for supersonic flight. Fuel components used for ducted rockets are fuel-rich propellant. To obtain high specific impulse, it is desired that the fuel materials evolve high combustion heat per unit mass in the air. Boron is the most suitable material of the fuel of ducted rockets in terms of its high combustion heat. Obtaining the combustion characteristics of boron particles is the key to improve boron particles combustion. In this study, combustion times of single particles and flame areas around the particles were measured by direct photography and spectroscopic analysis, and flame structure of burning particles was observed by schlieren photography. It was obtained that boron particles burn in two stages separately and the combustion time decrease with increasing temperature. The flame areas are composed with boron dioxide." @default.
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- W2332920001 date "2011-07-31" @default.
- W2332920001 modified "2023-09-27" @default.
- W2332920001 title "Combustion Characteristics of Boron Particles in The Secondary Combustor of Ducted Rockets" @default.
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- W2332920001 doi "https://doi.org/10.2514/6.2011-5867" @default.
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