A vertical take-off aircraft comprising a main power plant 1 at the top of the aircraft which consists of an assembly of blades 2, 3, a rotor 4 and a main engine assembly 5. The main power plant is connected to the main body 6 of the aircraft by a tilt enabling joint 7. The tilt enabling joint is connected to the main body by a telescopic tube assembly comprising tubes 12 and 13. To counter the rotational force exerted on the main body 6 of the aircraft by the rotation of the blades 2, 3, an additional power plant 15 is attached to the main power plant. Tilting the main power plant causes tilting of the additional power plant.
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