发明名称 ГЛОБАЛЬНАЯ СИСТЕМА КОНТРОЛЯ ПРОРЫВА БАЛЛИСТИЧЕСКИМИ РАКЕТАМИ ОГРАНИЧЕННОЙ СИСТЕМЫ ПРОТИВОРАКЕТНОЙ ОБОРОНЫ
摘要 FIELD: spacecraft control, applicable for control of additional launches of ballistic missiles in the conditions of penetration by them of the air defense system. ^ SUBSTANCE: the system has a Glonass functional navigation system including navigational satellites with an intersattelite communication equipment connected to the data transmission receiving and transmitting equipment, command post of strategic rocket forces connected to the ballistic missile launching system and having an equipment for reception of data of navigational satellites and ballistic missiles. The missile nose cones are provided with transducers, responding to unauthorized mechanical or beam actions and connected to the data transmission equipment. The mentioned transducers are made for transmission of information to the command post of strategic rocket forces via the intersatellite communication lines of the Glonass system on the mentioned action by means of the respective signals with a mark identifying the given ballistic missile. ^ EFFECT: provided monitoring of the state of the ballistic missiles in combat conditions, acceptance of a motivated decision on repeated launches compensating for the losses on the previous ones. ^ 1 dwg
申请公布号 RU2004131444(A) 申请公布日期 2006.04.10
申请号 RU20040131444 申请日期 2004.10.29
申请人 Закрытое акционерное общество "НПО Космического Приборостроени " (RU) 发明人 Урличич Юрий Матэвич (RU);Балуевский Юрий Николаевич (RU);Поповкин Владимир Александрович (RU);Черевков Константин Владимирович (RU)
分类号 F41H11/02;G08B25/10 主分类号 F41H11/02
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