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
Title | Year | Author | Number |
---|---|---|---|
AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2317922C1 |
AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2319644C2 |
AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2318700C1 |
AVIATION ROCKET COMPLEX | 2005 |
|
RU2359871C2 |
AIRCRAFT MISSILE COMPLEX | 2005 |
|
RU2309090C2 |
AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2319643C2 |
AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2314975C1 |
AIR ROCKET COMPLEX | 2009 |
|
RU2401779C1 |
AVIATION ROCKET COMPLEX | 2005 |
|
RU2359872C2 |
AVIATION ROCKET COMPLEX | 2005 |
|
RU2359873C2 |
Authors
Dates
2008-05-10—Published
2006-04-27—Filed