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Title: Precision guided antiaircraft munition

Patent ·
OSTI ID:866299

A small diameter, 20 mm to 50 mm, guided projectile is used in antiaircraft defense. A pulsing laser designator illuminates the target aircraft. Energy reflected from the aircraft is received by the guided projectile. The guided projectile is fired from a standard weapon but the spining caused by the riflings are removed before active tracking and guidance occurs. The received energy is focused by immersion optics onto a bridge cell. AC coupling and gating removes background and allows steering signals to move extended vanes by means of piezoelectric actuators in the rear of the guided projectile.

Research Organization:
Lawrence Livermore National Laboratory (LLNL), Livermore, CA (United States)
Assignee:
United States of America as represented by Secretary of Air (Washington, DC)
Patent Number(s):
US 4678142
OSTI ID:
866299
Country of Publication:
United States
Language:
English