FIELD: aeronautical and space engineering; space missile complexes with heavy ballistic missiles.
SUBSTANCE: proposed complex includes heavy ballistic missiles, more than 100 tons in mass which are equipped with liquid-propellant engines and are launched in air for injection of spacecraft into orbits. Aircraft missile complex includes, aircraft, airframe whose fuselage carries air-launching launch vehicle, device for mating the launch vehicle with aircraft performing the function of towing vehicles, systems ensuring their functioning and ground transportation and acceleration platform equipped with accelerating engine. Airframe fuselage may be separated over horizontal plane.
EFFECT: increased overall dimensions and launch weight of launch vehicle and consequently masses of spacecraft injected into orbits.
3 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2318700C1 |
AIRCRAFT MISSILE SYSTEM | 2006 |
|
RU2323854C2 |
AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2319643C2 |
AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2317922C1 |
AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2314975C1 |
AVIATION ROCKET COMPLEX | 2005 |
|
RU2359873C2 |
AVIATION ROCKET COMPLEX | 2005 |
|
RU2359872C2 |
AIRCRAFT MISSILE COMPLEX | 2005 |
|
RU2309090C2 |
AIR ROCKET COMPLEX | 2009 |
|
RU2401779C1 |
AVIATION ROCKET COMPLEX | 2005 |
|
RU2359871C2 |
Authors
Dates
2008-03-20—Published
2006-04-27—Filed