FIELD: aeronautical and space engineering; aircraft missile complexes with heavy missiles (more than 100 tons in mass) equipped with liquid-propellant engines and launched in air for injection of spacecraft into orbits.
SUBSTANCE: proposed aircraft missile complex includes aircraft, airframe with air-launched missile inside its fuselage, device for mating the launch vehicle with aircraft, systems ensuring their proper functioning and ground transportation and acceleration platform equipped with acceleration engines. Airframe fuselage is separable in construction; it may be separated over horizontal plane. Area of airframe wing may be changed after aircraft takeoff due to availability of separable parts of wing which are equidimensional and symmetrical in pairs relative to longitudinal axis of wing.
EFFECT: increased overall dimensions and launch weight of launch vehicle; increased masses of spacecraft injected into orbits.
3 cl, 1 dwg
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RU2323854C2 |
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RU2314975C1 |
AVIATION ROCKET COMPLEX | 2005 |
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AIRCRAFT MISSILE COMPLEX | 2005 |
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AIR ROCKET COMPLEX | 2009 |
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AVIATION ROCKET COMPLEX | 2005 |
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METHOD OF RESCUE OF AIRCRAFT ROCKET COMPLEX SPACE APPARATUS | 2011 |
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Authors
Dates
2008-02-27—Published
2006-04-27—Filed