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- W2320724352 abstract "The present thermal management system for a carrier-based Mach 5 cruise-capable aircraft whose propulsion system does not entail cryogenic fuels is predicated on the use of the catalytic endothermic reaction of a petroleum-derived hydrocarbon fuel as the heat sink for engine cooling. The insulation of engine flowpath surfaces reduces cooling requirements. The primary elements of this closed-cycle cooling system are a fuel preheater, a catalytic fuel reactor, and engine wall-cooling panels; a silicone-based liquid polymer is used as the coolant. Structural, weight, and thermal analysis results are presented for each of the primary components." @default.
- W2320724352 created "2016-06-24" @default.
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- W2320724352 date "1990-08-17" @default.
- W2320724352 modified "2023-10-14" @default.
- W2320724352 title "Thermal management for a Mach 5 cruise aircraft using endothermic fuel" @default.
- W2320724352 doi "https://doi.org/10.2514/6.1990-3284" @default.
- W2320724352 hasPublicationYear "1990" @default.
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