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Application filed by Zoran VardafiledCriticalZoran Varda
Priority to YU48299ApriorityCriticalpatent/YU48299A/en
Publication of YU48299ApublicationCriticalpatent/YU48299A/en
Hybrid antiaircraft defense is characterized by a rocket (6) fired out of a cannon with a flat tube (1) as under caliber projectile by means of a reductor (5), and in the final phase of the path, a rocket motor (6) is activated and a system for guiding that can be radar or infra red.
YU48299A1999-09-241999-09-24Hybride anti-air system
YU48299A
(en)