FIELD: aviation.
SUBSTANCE: space missile air-breathing launch system comprises a plinth, that is made of the upper non-rotatable ring with the support shafts for the space missile attached to this ring. The upper ring comprises the guidance system of the air-breathing launch system and the batteries of its energy supply. The upper ring leans on the lower rotatory ring by virtue of a magnetic bearing system. The blades are radially attached with one end to the lower ring. These blades are designed to generate the lift capacity of the air-breathing launch system. They also comprise the propellant components tanks. And at the far end the air breathing motors are attached to the blades for the blades about an axis swiveling that is perpendicular to the floating ring surface.
EFFECT: reliability and start efficiency growth.
7 dwg
Title | Year | Author | Number |
---|---|---|---|
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|
RU2620172C1 |
ELECTRICAL AIR START SYSTEM OF THE SPACE ROCKET | 2017 |
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RU2658236C1 |
AVIATION ROCKET COMPLEX | 2005 |
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RU2359872C2 |
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RU2323854C2 |
AIRCRAFT MISSILE COMPLEX | 2006 |
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RU2317922C1 |
AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2319643C2 |
AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2318700C1 |
AIRCRAFT MISSILE COMPLEX | 2006 |
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RU2314975C1 |
AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2319644C2 |
AIR ROCKET COMPLEX | 2009 |
|
RU2401779C1 |
Authors
Dates
2017-05-23—Published
2015-12-31—Filed