FIELD: armament, in particular, rocketry. SUBSTANCE: guided projectile has a control actuator, leading shaped charge, shaped-charge warhead, engine, control compartment with a gyro coordinator, stabilizers. The response time of the control electromagnet is within 0.1 to 0.25 of the response time of the control actuator unit. The speed of the control actuator unit is proportional to the projectile flight speed. The speed of projectile spinning is proportional to the projectile flight speed. EFFECT: enhanced accuracy of target hit. 3 dwg
Authors
Dates
2000-05-27—Published
1998-11-12—Filed