Designed to carry payloads of 25-30kg per rotor, with 54″ carbon propeller. Max thrust is up to 70kg per rotor, unit motor weighs only 2245g. With large pitch EVOTL CF propellers, achieving large load, high efficiency and excellent reliability, providing reliable power support for various endurance flights of professional UAVS.
Motor Data |
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| Motor Model | MAD V135L IPE V2.0 | Number of pole pairs | 19 |
| Stator | Anticorrosive | Varnished wire Degree | 220°C |
| Motor Size | D:144.6 × 66 mm | Magnet Degree | 180°C |
| Degree of Protection | IP35 | Cable Length | 150 mm (extended Enameled wires） |
| Centrifugal Heat Dissipation | YES | Rotor Balance | ≤10 mg |
| Propeller Mounting Holes | D:50 M6×6 | Motor Balance | ≤20 mg |
| Shaft Diameter | IN: 20 mm | Motor Mounting Holes | D:50 M6×4 |
| Bearing | 6904ZZ*2 | Disruptive test | 500 V |
| SOLUTION | ||
| VTOL Motor/KV | VTOL Prop | VTOL ESC |
| MAD V135L IPE 35KV | Fluxer Glossy 54x24 | MAD AMPX 300A(12-24S) |
| VTOL Battery(Lipo)/Voltage | VTOL Thrust Per Motor(kg) | The recommended takeoff weight(4 rotors) |
| 24S(4.3V/S)/84-104V | 25kg ~ 30kg | 112kg |
| Note:For a coaxial configuration, a total thrust loss of 25% should be considered. | ||
