Flying decoy

Details Flying decoy Flying decoy

1990-02-26

1994-05-31

Buczinski, Stephen C.

Radiant energy

Radiant energy generation and sources

Plural radiation sources

89 12, 102334, 102372, 102502, 102507, G01J 100, B64D 104, F41F 500, F42B 1000

Patent

active

053171632

ABSTRACT:
A decoy for misdirecting heat-seeking and radar-echo-seeking missiles comprised of as main components a radar reflector and an engine and capable of simulating an aircraft in the infra-red wavelength of 1.5 to 2.5 m.mu.; 3-5 m.mu.; and 8-14 m.mu. and simultaneously in the radar band. The decoy is spectrally adapted in the infra-red range and is contoured to exhibit a large reflective surface with a doppler effect in the radar band. The parts are constructed so that the desired configuration and aerodynamic stability is achieved only when the decoy is prepared for operation. A plume covering an appropriately large area is produced and the content of the exhaust includes carbon dioxide and/or metallic powder to a high IR radiation of the plume.

REFERENCES:
patent: 1803537 (1931-05-01), Nissen
patent: 2498080 (1950-02-01), Jasse
patent: 3413636 (1968-11-01), Migdal
patent: 3866226 (1975-02-01), Benneche et al.
patent: 3946555 (1976-03-01), Goede
patent: 3986909 (1976-10-01), Macri
patent: 4318270 (1982-03-01), Orlick et al.
patent: 4428583 (1984-01-01), Feagle

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