FIELD: flight vehicle.
SUBSTANCE: invention relates to pace engineering and can be used in carrying cargoes in both outside space and atmosphere. The flight vehicle consist of rigidly coupled airframe ands a cylinder, a piston accommodated in the said cylinder, two exhaust pipes rigidly coupled with the cylinder and two safety stops. The said flight vehicle is furnished with a solid-propellant damper, a damper fuel charge igniter, a jet solid-propellant piston engine, a piston jet engine fuel charge igniter. The solid-propellant damper is rigidly attached to the cylinder and arranged ahead the piston. The said damper electrical input is connected to that of the damper fuel charge igniter, the damper being rigidly fixed to the airframe, while the piston jet solid-propellant engine is rigidly coupled with the piston, and its electrical input is connected to the output of the fuel charge igniter of the aforesaid jet solid propellant piston engine.
EFFECT: simpler design of the flight vehicle and higher reliability.
1 dwg
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RU2134218C1 |
FLYING VEHICLE | 2006 |
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RU2307773C1 |
SPACECRAFT | 2011 |
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RU2451630C1 |
AIRCRAFT | 2015 |
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RU2600259C1 |
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RU2281889C1 |
FLYING VEHICLE | 2005 |
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RU2297953C1 |
Authors
Dates
2008-07-27—Published
2006-11-27—Filed