Product overview
The MAD V135L IPE EVTOL Drone Motor is a propulsion component for professional UAVs, with the motor identified as MAD V135L IPE V2.0. It is designed to carry 25–30kg per rotor with a 54-inch carbon propeller, while maximum thrust is stated as up to 70kg per rotor. The unit motor weighs 2245g. Its physical construction combines an anticorrosive stator, 19 pole pairs, two 6904ZZ bearings and centrifugal heat dissipation within a D:144.6 × 66 mm motor envelope.
Integration provisions include separate D:50 M6×6 propeller and D:50 M6×4 motor mounting patterns, an internal shaft diameter of 20 mm and 150 mm extended enameled wires. The motor has IP35 protection, with wire and magnet temperature ratings of 220°C and 180°C respectively. The 35KV-24S solution pairs it with a Fluxer Glossy 54x24 propeller and MAD AMPX 300A(12-24S) ESC; these are solution components rather than an explicit bundled supply list. Recommended four-rotor takeoff weight is 112kg, and coaxial installation requires allowance for 25% total thrust loss.
Specifications
| Specification | Value & conditions |
|---|---|
| Motor model | MAD V135L IPE V2.0 |
| Number of pole pairs | 19 |
| Stator | Anticorrosive |
| Varnished wire temperature rating | 220°C |
| Motor size | D:144.6 × 66 mm |
| Magnet temperature rating | 180°C |
| Degree of protection | IP35 |
| Cable length | 150 mmExtended 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 |
| Bearings | 6904ZZ*2 |
| Disruptive test voltage | 500 V |
| KV option | 35KV |
| Designed payload per rotor | 25-30kg per rotorWith a 54″ carbon propeller. |
| Maximum thrust | Up to 70kg per rotor |
| Motor weight | 2245gUnit motor. |
| Recommended propeller | Fluxer Glossy 54x2435KV-24S solution. |
| Recommended ESC | MAD AMPX 300A(12-24S)35KV-24S solution. |
| Battery configuration and voltage | 24S(4.3V/S)/84-104V35KV-24S solution; LiPo battery. |
| Solution thrust per motor | 25kg ~ 30kg35KV-24S solution with Fluxer Glossy 54x24 propeller and MAD AMPX 300A(12-24S) ESC. |
| Recommended takeoff weight | 112kgFour rotors in the 35KV-24S solution. |
| Total thrust loss allowance | 25%Coaxial configuration. |
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