Study on Flight Performance of Propeller-Driven UAV

Table 3

The main parameters of UAV.

Length	8.13 m	Wing area	11.45 m^2
Maximum width at the front of the fuselage	1.12 m	Height	2.21 m
Maximum width behind the fuselage	0.75 m	Tail wing	4.38 m
Propeller diameter	1.73 m	Aircraft upper body area	19.17 m^2
Empty weight	350 kg	Weight of fuel	295 kg
Maximum task load	204 kg	Maximum takeoff weight	1020 kg