Split flow injector for solid fuel ramjets

Details Split flow injector for solid fuel ramjets Split flow injector for solid fuel ramjets

1976-08-06

1977-06-28

Freeh, William L.

Power plants

Reaction motor

Solid and fluid propellant

60270S, 60 3972R, F02K 904

Patent

active

040316980

ABSTRACT:
A split flow injector for solid fuel ramjets (SFRJ) having a tube injected nto the injector port of a SFRJ to split the air into two streams wherein the primary airflow through the annular area around the tube is injected into the recirculation region just inside the injector port to stabilize combustion.

REFERENCES:
patent: 2799987 (1957-07-01), Chandler
patent: 3038303 (1962-06-01), Gose
patent: 3555826 (1971-01-01), Bennett

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