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Aircraft has front longitudinal section to receive cockpit area, rear longitudinal section to receive rear body section and central longitudinal section to receive intermediate region of body between cockpit area and rear body section
Aircraft has front longitudinal section to receive cockpit area, rear longitudinal section to receive rear body section and central longitudinal section to receive intermediate region of body between cockpit area and rear body section
The aircraft has a body (10), made of metallic materials and composite materials, is provided with wings (30), where multiple openings (21,22,23,24,25,26,27) in the body. Coupling points (31,41,51) are provided for wings on the body, where the body is divided into three longitudinal sections. The front longitudinal section receives a cockpit area (11), where the rear longitudinal section receives a rear body section (13) of the body. The central longitudinal section receives an intermediate region (12) of the body between the cockpit area and the rear body section.
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