Heavy Lift Multirotor UAV - Electric Propulsion Unit Experimental Data

Experimental measurement data was obtained utilizing RCbenchmark 1780 with full-range PWM signals. Measurements were made for two series of setups.First series is related to low-voltage setups using the following T-MOTOR components: - motors: MN4014 400Kv, MN5212 340Kv, MN501-S 360Kv, U7 280Kv, MN6007 320Kv, P60 340Kv, MN701-S 280Kv; - ESC: Air 40A, Flame 40A, Flame 70A, Alpha 60A, Flame 100A; - propellers: P17×5.8, P18×6.1, P20×6, P22×6.6, P24×7.2, G26×8.5; - battery: 6-cell (6S) Lithium polymer (LiPo).The second series is related to high-voltage setups using the following T-MOTOR components: - motors: AG1005 90Kv, U11 120Kv, P80 100Kv, U12 120Kv, U13 130Kv; - ESC: Flame 60A, Alpha 80A, Alpha 120A, Flame 180A; - propellers: G26×8.5, G28×9.2, G30×10.5, G32×11.0; - battery: 12-cell (12S) (LiPo).