FIELD: aerospace engineering.
SUBSTANCE: invention relates to aerospace engineering, particularly, to flight vehicle power plants for flights in atmosphere and open space. Proposed flight vehicle comprises the body, cone-like combustion chamber with exhaust nozzle arranged at the body rear and combustion chamber control unit communicating with the said chamber. Bent exhaust pipes and two jet engines are rigidly attached to the body. Aforesaid combustion chamber features rounded recess arranged at the body front with two additional exhaust nozzles arranged on both sides of the said recess and turned apart relative to each other. These nozzles communicate with aforesaid combustion chamber and appropriate exhaust pipes. Note that the body is provided with a ledge rigidly jointed thereto to accommodate aforesaid combustion chamber and exhaust nozzle. Two jet engines are arranged right behind the said ledge.
EFFECT: reduced overall dimensions.
1 dwg
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Authors
Dates
2009-08-10—Published
2008-06-03—Filed