发明名称 АВИАЦИОННЫЙ РАКЕТНЫЙ КОМПЛЕКС
摘要 FIELD: engines and pipes. ^ SUBSTANCE: aircraft missile system contains airplanes, airframe, in the fuselage of which it is disposed the booster rocket of airborne device of mating the booster rocket with the airplane, making the function of the towing vehicle, and systems providing their functioning, and surface-mounted transport-booster platform, equipped with engines for its boosting. On the rocket fuselage it is additionally installed the cowling with additional wing on it, and brad with tail cowling. On the tail cowling it is installed the stabilization device and rudder unit. The cowlings are made with possibility of being removed from the rocket. ^ EFFECT: it is achieved the exceeding of the distance of flight and it is arisen the cargo mass of space objects bringing to the orbit. ^ 3 cl, 1 dwg
申请公布号 RU2006114563(A) 申请公布日期 2007.11.20
申请号 RU20060114563 申请日期 2006.04.27
申请人 Федеральное государственное унитарное предпри тие"Государственный ракетный центр "КБ им. академикаВ.П. Макеева" (RU) 发明人 Данилкин В чеслав Андреевич (RU);Дегт рь Владимир Григорьевич (RU);Сабуренко Валерий Васильевич (RU);Шевалдина Лариса Витальевна (RU)
分类号 B64G1/00 主分类号 B64G1/00
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