Rocket drive with air intake

Power plants – Reaction motor – Liquid oxidizer

Patent

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Details

60260, 602701, F02K 948

Patent

active

047716010

ABSTRACT:
A rocket propulsion system working with cryogenic fuel is modified by supersonic and hypersonic flight wherein air is sucked in to be used in lieu of the oxidizer in the rocket system. Hybrid operation is provided for.

REFERENCES:
patent: 2735263 (1956-02-01), Charshafian
patent: 2883829 (1959-04-01), Africano
patent: 2948112 (1960-08-01), Smith
patent: 2960834 (1960-11-01), Kirkpatrick
patent: 3002340 (1961-10-01), Landerman
patent: 3040519 (1962-06-01), Rae
patent: 3040520 (1962-06-01), Rae
patent: 3561217 (1971-02-01), Hall
patent: 3775977 (1973-12-01), Builder et al.

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