Aircraft Capable Of Hovering

An aircraft comprising:

• a propulsion unit with a first rotor for providing a propulsion force on the aircraft;
• a fuselage unit extending along a rotation axis of the first rotor and having a rotational symmetrical shape with respect to the rotation axis of the first rotor;
• wherein the fuselage unit has a suspension at a first end by which the fuselage unit is coupled to the first rotor so that the fuselage unit is spaced apart from the first rotor along the rotation axis;
• wherein a detection unit for the detection of environmental information is provided in the area of a second end of the fuselage unit;
• wherein the propulsion unit is configured to keep the aircraft in a hovering flight condition, so that a relative position of the aircraft with respect to a reference point on the Earth's surface remains unchanged;
• and
• wherein the first rotor has at least two rotor blades, whose profile shape remains unchanged over a longitudinal extension direction of the rotor blades.