Electric flight vehicle

An electric flight vehicle comprising:

• an airframe;
• a central propulsor that is disposed in a region including a gravity center position of the airframe in a plan view and that includes an electric motor, a fan which is rotationally driven by the electric motor, and a tubular duct which covers the fan from an outer periphery side;
• a manifold that is connected to an outlet of the central propulsor and that extends in a plurality of different directions to divert an airflow in the plurality of directions;
• a thrust vectoring unit that is provided at each outlet of the manifold and that thrust-vectors the airflow;
• a thrust vectoring actuator unit that controls an angle of the thrust vectoring unit;
• a cargo platform that is provided above the central propulsor and that has a loading surface on which cargo is loaded;
• a supporting part that connects the cargo platform to the airframe, and
• a fairing portion that is provided to be rotatable with respect to the supporting part around a rotation axis with an extending direction of the supporting part as an axis, and that has an airfoil-shaped cross-sectional shape when viewed from a direction of the rotation axis.