发明名称 СПОСОБ СТРЕЛЬБЫ УПРАВЛЯЕМЫМ АРТИЛЛЕРИЙСКИМ РЕАКТИВНЫМ СНАРЯДОМ С САМОНАВЕДЕНИЕМ НА КОНЕЧНОМ УЧАСТКЕТРАЕКТОРИИ ПОЛЕТА И УСТРОЙСТВО ДЛЯ ЕГО РЕАЛИЗАЦИИ
摘要 FIELD: rocketry. ^ SUBSTANCE: the method consists in launching of the projectile from the gun barrel in a mortar trajectory and start of the jet engine in the trajectory of its flight. At and outrange fire the jet engine is started in the upward leg of the projectile flight trajectory. At a short-range fire the jet engine is started in the downward leg of the projectile flight trajectory. The projectile for realization of the method has a jet engine with a pyrotechnic igniter and an electronic equipment programmed before the start. The electronic equipment is provided with a timer for the start of the jet engine in the upward or downward leg of the projectile flight trajectory. ^ EFFECT: expanded functional potentialities of projectiles with homing in the terminal flight leg. ^ 2 cl, 3 dwg
申请公布号 RU2006102930(A) 申请公布日期 2007.08.20
申请号 RU20060102930 申请日期 2006.02.01
申请人 Государственное унитарное предпри тие "Конструкторское бюро приборостроени " (RU) 发明人 Бабичев Виктор Ильич (RU);Захаров Владислав Львович (RU);Сабинин Сергей Владимирович (RU);Лопатин Константин Константинович (RU)
分类号 F42B15/00 主分类号 F42B15/00
代理机构 代理人
主权项
地址