FIELD: rocketry and space engineering.
SUBSTANCE: invention can be used in space aircraft missile complexes, mainly with heavy ballistic missiles, mass exceeding 100 tons, furnished with liquid-propellant rocket engines and launched in air for orbit injection of spacecraft. Proposed aircraft missile complex contains aircraft, airframe with air start launch vehicle located inside fuselage, device for matching launch with aircraft playing part towing tugs, system providing their functioning and ground transportation-acceleration platform with its acceleration engines. Fuselage of airframe is made for division along horizontal plane. Transportation acceleration platform is essentially aircraft with residual service life and resource and modified for arrangement and ground transportation of airframe with launch vehicle and for operation in aircraft missile complex.
EFFECT: possibility to increase overall dimensions and takeoff weight of launch vehicle and, as result, to increase orbit injected masses of spacecraft.
4 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2319644C2 |
| AIRCRAFT MISSILE SYSTEM | 2006 |
|
RU2323854C2 |
| AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2319643C2 |
| AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2314975C1 |
| AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2317922C1 |
| AVIATION ROCKET COMPLEX | 2005 |
|
RU2359872C2 |
| AIR ROCKET COMPLEX | 2009 |
|
RU2401779C1 |
| AVIATION ROCKET COMPLEX | 2005 |
|
RU2359873C2 |
| AIRCRAFT MISSILE COMPLEX | 2005 |
|
RU2309090C2 |
| AIRCRAFT MISSILE SYSTEM | 2006 |
|
RU2323856C2 |
