FIELD: aviation. SUBSTANCE: proposed flying vehicle has two fuselages interconnected by means of wing in tail section and by means of horizontal unit in nose section, vertical tail unit, power plant and landing gear. Fuselages are interconnected by means of center-wing section in tail section without extending beyond trailing edge of wing. Nose horizontal planes have low fineness ratio. According to second variant, vertical tail unit consists of two fins mounted in inclined position of center-wing section. Fins are connected with fairing. One fin or both fins are articulated on center- wing section for turn relative to axis which is parallel to axis of symmetry of flying vehicle; one fin is detachably connected with fairing. Provision is made for all-round view of radar station in azimuth. EFFECT: enhanced efficiency. 22 cl, 8 dwg
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Authors
Dates
2003-09-27—Published
2002-07-18—Filed