Аванпроєкт ближньомагістрального літака вантажопідйомністю до 6000 кг

Abstract

Object of the design is development of the short-range aircraft with commercial cargo payload capacity up to 6000 kg. Aim of the diploma work is the development of the aircraft preliminary design and characteristic estimation. The method of design is analysis of the prototypes and selections of the most advanced technical decisions. The diploma work contains drawings of design of the short-range aircraft with commercial cargo payload capacity up to 6000 kg, calculations and drawings of the aircraft layout, the cargo compartment and equipment.