A dual flow path exhaust assembly for use with a combined turbofan and ramjet engine includes a turbofan engine exhaust duct, a ramjet engine exhaust duct, a combined outlet, and door configured to move between an open position and a closed position to selectively isolate the turbofan engine exhaust duct from the combined outlet.
Dual flowpath exhaust for fuel cooling in a hypersonic propulsion system
2022-05-24
Patent
Electronic Resource
English
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