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. The fuselage of the airframe is made with possibility of its dividing in horizontal plane. The wing of the airframe is made with possibility of its surface changing after the lifting-off. The changing of the wing surface is achieved thanks to separately fixed wings parts, equal by pairs and symmetrical disposed relatively to longitudinal axis of the wing, connected with each other with possibility of separation from the wing of the airframe. ^ EFFECT: it is achieved the extension of the sizes and start weight of the booster rocket, and thanks to it is arisen the cargo mass of space objects bringing to the orbit. ^ 3 cl, 3 dwg
申请公布号 RU2006114560(A) 申请公布日期 2007.11.10
申请号 RU20060114560 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);Карпов Анатолий Степанович (RU)
分类号 B64G1/14 主分类号 B64G1/14
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