Reverse flow aft inlet ramjet system

Details Reverse flow aft inlet ramjet system Reverse flow aft inlet ramjet system

1975-03-11

1976-12-21

Freeh, William L.

Power plants

Reaction motor

Motive fluid from diverse generators alternatively ejected...

60270R, F02K 902, F02K 710

Patent

active

039980502

ABSTRACT:
A combined rocket/ramjet for propelling a missile including a missile payload module and an integral rocket/ramjet engine system strapped on the missile payload module, and incorporating a liquid fuel rocket engine and a ramjet engine having a combustion chamber common with the rocket engine, an exhaust nozzle, and multiple aft-mounted air inlets movable between a retracted position during rocket boost flight and an extended, pop-out position to receive and direct ram air in a reverse flow direction into the combustion chamber during ramjet flight.

REFERENCES:
patent: 2417445 (1947-03-01), Pinkel
patent: 2799987 (1957-07-01), Chandler
patent: 2977753 (1961-04-01), Boulet
patent: 3038408 (1962-06-01), Kluge
patent: 3112903 (1963-12-01), Conrad
patent: 3482403 (1969-12-01), Polk, Jr.
patent: 3802192 (1974-04-01), Curran

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