FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering. Airborne vehicle comprises airframe, air intake, control unit and conical combustion chamber with exhaust nozzle. Airframe is rigidly coupled with control unit and conical combustion chamber. Combustion chamber has two hydraulic links with control unit and is rigidly coupled with exhaust nozzle.
EFFECT: decreased overall dimensions, sufficient acceleration.
1 dwg
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