FIELD: rocket armament. SUBSTANCE: the projectile has a jet engine, detachable nose cone, separation and breakaway device. The breakaway device is made in the form of two masses opposite-arranged relative to the longitudinal axis. One of them is positioned in the engine, and the other - in the nose section. The masses are unilaterally shifted in the longitudinal direction relative to the center of mass of the engine and nose section respectively. EFFECT: enhanced reliability of combat use of projectile due to prevention of collision of the engine and nose section after their separation. 3 dwg
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Authors
Dates
1999-09-27—Published
1998-05-05—Filed