Pre-combustion integrated Ram airbreathing laser

Coherent light generators – Particular pumping means – Gas dynamic

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Details

372701, 372 77, 372 58, H01S 309

Patent

active

047138238

ABSTRACT:
The present invention provides a Ram airbreathing laser adapted to use with an aircraft which operates primarily in the Mach 3 to Mach 6 regime. Valves, or gates, are provided in the propulsive flow path and the auxiliary flow path for laser in a manner such that the air entering the aircraft engine inlet duct system is either directed to the laser or to the propulsive flow path depending upon the desired mode of operation of the aircraft.

REFERENCES:
patent: 4013976 (1977-03-01), Hill et al.

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