An aerodynamic apparatus containing an external body able to provide for a motion of a gaseous operation medium, such as air, and to use controlled reaction forces of the gaseous operation medium for various maneuvers; with fan blowers each respectively comprising a first and second drive motor (1, 22); a primary wing and a steering wing; a system for gaseous operation medium temperature control (28, 29, 30); an external communication unit (13, 14, 15, 16, 23, 24, 26, 27) with openings in the external body, whereby the functions of the external communication unit are performed by appropriate valves (13, 15, 23, 26); characterized in that the external body of the apparatus is sphere shaped; inside the external body there is a sphere shaped middle body which is rigidly connected to the external body with fastening means, with space α between these bodies (17, 19); inside the middle body there is a sphere shaped internal body which is rigidly connected to the middle body with fastening means, with space β between the middle body and the internal body and with a space γ within the internal body; in the space γ there is the main fan with the first drive motor, which is rigidly connected to the internal body by a supporting means of the main fan, comprising the primary wing which is made in a petal-like shape with annular rotary means provided with a motor including drive assemblies of the annular rotary means for annular rotation of the primary wing around an apparatus axial axis (O-O) and with supporting means of the primary wing; on the surface of the internal body on a side of a trailing edge of the primary wing there is an opening connecting spaces γ and β for the operation medium which is regulated by a rear bypass valve of the middle body, the bypass valve being controlled by a motor with drive assemblies of the rear bypass valve of the middle body; the apparatus is provided with the system for operating medium temperature control (28, 29, 30) having the following arrangement of its main units: - a cooling facility comprising - a compressor which is rigidly mounted in space α, - an evaporator with a throttle valve, which is rigidly mounted in space β, and - a condenser-radiator which is rigidly mounted on a rear outer hemisphere of the external body; along an axial axis of the main fan with a first drive motor on the middle body there is the peripheral fan, for directing the operation medium back to the main fan, with the second drive motor rigidly mounted in coaxial alignment; in space β along the axial axis (O-O) of the main fan with the first drive motor there is a front bypass valve of the internal body driven by a motor with drive assemblies of the front bypass valve of the internal body that allows for controlling air travel from space β to space γ, wherein on the surface of the internal body there is an internal body front bypass valve seal which, for the closed position of front bypass valve of the internal body, allows for proper pressurization and prevents air travel from space β to space γ; in the direction of the flow of the operation media, coming off the primary wing, along the axial axis of the fans (1, 22) on the middle body there is a rear shutter valve driven by a motor with drive assemblies of the rear shutter valve and used to control air travel from space γ to the atmosphere; along the axial axis (O-O) of the fans (1, 22) behind the rear shutter valve there is the steering wing for interaction with operation medium that flows outwardly from the internal space γ towards the atmosphere made in a petal-like shape with annular rotary means of the steering wing for annular rotation around an apparatus axial axis (O-O) provided with a motor with drive assemblies of the annular rotary means of the steering wing and supporting means of the steering wing; along the axial axis of the fans (1, 22) in space α there is a front bypass valve of the middle body driven by a motor with drive assemblies of the front bypass valve of the middle body and used to control the air travel from the external atmosphere to spaces α and γ consecutively; in the inter-body spaces of the apparatus there are facilities of the condensate collecting and draining system which is provided with a drain pump with a discharge tube; in the lower part of the external body of the apparatus there is a retractable landing gear provided with landing gear motors with drive assemblies, in so doing, for the landing gear retracted position, the lower part of the external body has an indention designed in such a manner that, with the help of the indention, the retracted landing gear fits the external body structure, thus minimizing the free air aerodynamic drag when it flows around the external body; the middle body contains an attitude orientation system and an automated control system. - a cooling facility comprising - a compressor which is rigidly mounted in space α, - an evaporator with a throttle valve, which is rigidly mounted in space β, and - a condenser-radiator which is rigidly mounted on a rear outer hemisphere of the external body;