FIELD: transport engineering. SUBSTANCE: vehicle has fuselage with a horizontal tail unit and load-carrying wing with flaps and motors secured to the fuselage. The motors are connected with propellers. The end faces of the wing are provided with side members. The bottom portions of the members and fuselage are provided with buoyant chambers. The load-carrying wing is rectangular. The horizontal tail unit is mounted above the wing. EFFECT: enhanced efficiency.
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Authors
Dates
1996-07-27—Published
1990-05-14—Filed