FIELD: armament; rocketry.
SUBSTANCE: proposed actuator unit has armature located perpendicularly relative to longitudinal axis of projectile; in central part of armature there is port for free passage of cumulative jet. Cores with coils secured to frame are mounted on both sides from port along projectile axis; distance between cores and coils is equal to width of armature port.
EFFECT: enhanced piercing effect due to reduced length of actuator unit.
2 dwg
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Authors
Dates
2004-08-20—Published
2003-03-11—Filed