Two-stage hypersonic ramjet

Details Two-stage hypersonic ramjet Two-stage hypersonic ramjet

1975-09-04

1982-07-13

Bentley, Stephen C.

Power plants

Reaction motor

Interrelated reaction motors

60270R, F02K 718, F02K 976

Patent

active

043387837

ABSTRACT:
A two-stage ramjet engine including an aft end, ejectable, boost stage-combustor
ozzle assembly for initially accelerating from low-to-mid-supersonic launching speeds to high supersonic speeds, and mounted in a tandem arrangement immediately aft of a separate, forward end-cruise stage-combustor
ozzle assembly positioned directly behind an inlet-diffuser section for subsequently further accelerating from high supersonic to hypersonic speeds after ejecting the entire boost stage.

REFERENCES:
patent: 2540594 (1951-02-01), Price
patent: 2570629 (1953-10-01), Anxionnaz et al.
patent: 2644396 (1953-07-01), Billman
patent: 2684629 (1954-07-01), Nordfors
patent: 2686473 (1954-08-01), Vogel
patent: 2766581 (1956-10-01), Welsh
patent: 2995892 (1961-08-01), Kosson et al.
patent: 3066480 (1962-12-01), Buck
patent: 3067573 (1962-12-01), Connors

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