Preliminary Design for a Jet Training Aircraft

Abstract This paper present the results of our project to develop preliminary design a jet trainer plane (JTP) with two-person crew, base version which is intended for cadet training. We first consider assumptions and requirements new aircraft, review parameters existing aircraft designs in similarly-purposed class. Next we argue certain choices, regarding layout, cockpit configuration, wing location wingform, tail scheme, powerplant. The resulting calculated have maximum flight speed 940 km/h, ground-level rate climb 100 m/s, range 1130 km. plane’s take-off mass calculated, three approximations, at 2264 kg. Lastly training geometrical parameters, general view, master geometry.