Development of Dual Power Multirotor System

Table 2

Various flight configurations.

Flight condition	Maximized endurance	Balanced	Maximized payload
Empty weight	19.6 kg	19.6	19.6
Fuel load	3.2 kg	1.6	1
Battery weight	12.8 kg	12.8	12.8
Payload	0 kg	12	20
Total weight	36 kg	46.4	53.8
Engine thrust	24 kg	28	29
Motor thrust	12 kg	18.4	24.8
Endurance	60 min	28	20