Aircraft sighting system

Ordnance – Mounts – Training mechanisms

Patent

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Details

89 4106, 89 4107, 348167, 342 66, 342 67, F41G 518

Patent

active

054838657

ABSTRACT:
The present invention relates to a sighting system for an aircraft, in particular a rotary wing aircraft such as a helicopter. According to the invention, the sighting system comprises, in combination, an observation first individual apparatus integrated in the sides of the aircraft, and an axial fire second individual apparatus integrated at the front of aircraft, said first and second apparatuses being connected to the onboard computer of the aircraft.

REFERENCES:
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patent: 3641261 (1972-02-01), Chaplin et al.
patent: 3711638 (1973-01-01), Davies
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patent: 4202246 (1980-05-01), Schertz et al.
patent: 4779095 (1988-10-01), Guerreri
patent: 5223839 (1993-06-01), Grossman
patent: 5359920 (1994-11-01), Muirhead et al.
Keirstead et al, "Aircraft Survivability in the 21st Century-ATIRCM", Journal of Electronic Defense, May 1992.

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