Missile guidance system using an injection laser active missile

Details Missile guidance system using an injection laser active missile Missile guidance system using an injection laser active missile

1968-02-23

1976-05-04

Wilbur, Maynard R.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

250203R, 250338, F41G 700, G01J 120

Patent

active

039542289

ABSTRACT:
A missile guidance system utilizing an integrated active missile infrared eker including an injection laser transmitter, a semiconductor detector and a conical scanning acquisition and guidance system.

REFERENCES:
patent: 3504979 (1970-04-01), Stephany

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