Product overview
The MAD V122L eVTOL Drone Motor is a propulsion component for professional UAV endurance flights, with the motor identified as MAD V122L IPE V2.0 and offered in 36KV form. Its 144.6 × 53 mm body weighs 1620g and incorporates an anticorrosive stator, centrifugal heat dissipation and two 6904ZZ bearings. Integration provisions include a 20 mm internal shaft diameter, separate D:50 M6×6 propeller and D:50 M6×4 motor mounting patterns, and 150 mm extended enameled wires. The protection rating is IP35.
The motor is intended to carry 18–21kg per rotor with a 47.5-inch carbon propeller, while maximum thrust is stated separately as up to 50kg per rotor. A listed VTOL solution pairs the 36KV motor with Fluxer VTOL 40x13.1/42x14 propellers, a MAD AMPX 120A(12-24S) ESC and a 24S LiPo specification of 4.3V/S and 84–52V. That configuration specifies 16–20kg thrust per motor and a recommended 76kg takeoff weight for four axes. Coaxial installations require a 25% total thrust loss allowance.
Specifications
| Specification | Value & conditions |
|---|---|
| Motor model | MAD V122L IPE V2.0 |
| Number of pole pairs | 19 |
| Stator | Anticorrosive |
| Varnished wire temperature rating | 220°C |
| Motor size | D:144.6 × 53 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 | 36KV |
| Designed payload per rotor | 18-21kg (39.6bl-46.29bl)With a 47.5″ carbon propeller. |
| Maximum thrust per rotor | Up to 50kg(110.23bl) |
| Unit motor weight | 1620g |
| Solution motor | MAD V122L IPE 36KVListed VTOL solution. |
| Solution propeller | Fluxer VTOL 40x13.1/42x14Listed VTOL solution. |
| Solution ESC | MAD AMPX 120A(12-24S)Listed VTOL solution. |
| Solution battery and voltage | 24S(4.3V/S)/84-52VListed VTOL solution; LiPo battery. |
| Solution thrust per motor | 16kg ~ 20kgListed VTOL solution with Fluxer VTOL 40x13.1/42x14 propeller, MAD AMPX 120A(12-24S) ESC and 24S(4.3V/S)/84-52V LiPo battery. |
| Recommended takeoff weight | 76kgFour-axis configuration using the listed VTOL solution. |
| Total thrust loss allowance | 25%Coaxial configuration. |
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