FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Propulsive wing is composed of hollow frame formed by front, rear, top and bottom and lateral wall and filled with gas. Front and rear wall of said frame are rigid and interconnected while bottom and rear walls form elastic web tightly connected with bottom edge of front and rear edge of top wall and with lateral walls. Pulsed heat generator is arranged between front and top walls inside said frame and comprises fuel feed nozzle to create fuel-air mix nearby front wall inner surface and mix ignition system. Front wall has inlet opening with outside air inlet valve while rear wall is provided with used gas discharge opening.
EFFECT: takeoff and landing without run.
2 cl, 2 dwg
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