FIELD: aircraft engineering.
SUBSTANCE: invention relates to aerospace engineering and can be incorporated with aerospace vehicles equipped with liquid propellant engines and launched from aboard the aircraft to place a spacecraft into orbit. The proposed complex comprises an aircraft, wingless rocket-carrier, rocket-carrier-to-aircraft coupling assembly, systems maintaining the complex serviceability and a surface transport-and-boosting platform furnished with engines. Note that the rocket-carrier accommodates additionally a fairing with a wing, nose and tail cones, the latter being furnished with a fin and vertical unit. Aforesaid cones can be separated from the rocket-carrier body. Integrated strap cord, wing, center wing and its fairing make a rocket-carrier-to-aircraft coupling assembly. The said surface transport-boosting platform represents an aircraft sufficient operating hours, adapted for accommodation and surface transportation of rocket-carrier.
EFFECT: larger sizes and weight of rocket-carrier and, hence, increased weight of space apparatuses to be place into orbit.
3 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRCRAFT MISSILE SYSTEM | 2006 |
|
RU2323856C2 |
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|
RU2323855C2 |
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RU2317920C1 |
AIR ROCKET COMPLEX | 2009 |
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AVIATION ROCKET COMPLEX | 2005 |
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RU2359881C2 |
AVIATION ROCKET COMPLEX | 2005 |
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AVIATION ROCKET-LAUNCHING COMPLEX | 2005 |
|
RU2345927C2 |
Authors
Dates
2009-05-20—Published
2006-04-27—Filed