Product overview
The MAD V62 eVTOL Drone Motor is a propulsion component for professional industrial fixed-wing eVTOL UAS in the 15-20kg MTOW class, intended for large-pitch 18–22-inch carbon-fiber propellers. The motor designation is MAD V62 IPE V1.0, with 210KV and 280KV options. Each motor weighs 270g, and maximum thrust reaches up to 11.5kg per rotor. Its physical construction combines 14 pole pairs, an anticorrosive stator, two 6801ZZ bearings and centrifugal heat dissipation, with an IP35 protection rating.
Mechanical integration centers on a D:72 × 33.5 mm motor body. Motor mounting holes are D:25 M3×4 and D:30 M3×4, while the propeller interface provides D:12 M3×4, 18 M3×4 and 22 M3×4 patterns. The shaft diameter entry is IN: 12 mm. Electrical connection uses an 80mm black silicone cable in 16# AWG. Rotor balance is ≤5 mg and motor balance is ≤10 mg. The varnished wire degree is 180°C, and the disruptive test rating is 500 V.
The 210KV propulsion combination uses a Fluxer VTOL 22.1x7.4 propeller and MAD AMPX 80A (5-14S) ESC, with 4kg~6kg thrust per motor and a recommended takeoff weight of 20kg. The 280KV combination pairs a FLUXER VTOL 18.1X7.2 propeller with the same ESC, with 4kg~5kg per motor and a recommended takeoff weight of 19kg. Both combinations specify LiPo 12S(4.3V/S)/42-52V power. A coaxial installation requires allowance for a 25% total thrust loss.
Specifications
| Specification | Value & conditions |
|---|---|
| Intended aircraft MTOW | 15-20kgFor professional industrial eVTOL fixed-wing UAS with large-pitch 18–22-inch carbon-fiber propellers. |
| Maximum thrust per rotor | Up to 11.5kg |
| Motor weight | 270gPer motor. |
| Motor model | MAD V62 IPE V1.0 |
| Number of pole pairs | 14 |
| Stator | Anticorrosive |
| Varnished wire degree | 180°C |
| Motor size | D:72 × 33.5 mm |
| Motor balance (temperature entry) | 150°C |
| Degree of protection | IP35 |
| Cable length and construction | 80mm 16# Awg(Black) silicone |
| Centrifugal heat dissipation | YES |
| Rotor balance | ≤5 mg |
| Propeller mounting holes | D:12 M3×4, 18 M3×4, 22 M3×4 |
| Motor balance | ≤10 mg |
| Shaft diameter | IN: 12 mm |
| Motor mounting holes | D:25 M3×4, D:30 M3×4 |
| Bearing | 6801ZZ*2 |
| Disruptive test | 500 V |
| KV options | 210KV 280KV |
| 210KV propeller and ESC | Fluxer VTOL 22.1x7.4; MAD AMPX 80A (5-14S)V62 210KV propulsion configuration. |
| 210KV battery, thrust and recommended takeoff weight | LiPo 12S(4.3V/S)/42-52V; thrust per motor 4kg~6kg; recommended takeoff weight 20kgV62 210KV with Fluxer VTOL 22.1x7.4 propeller and MAD AMPX 80A (5-14S) ESC. |
| 280KV propeller and ESC | FLUXER VTOL 18.1X7.2; MAD AMPX 80A (5-14S)V62 280KV propulsion configuration. |
| 280KV battery, thrust and recommended takeoff weight | LiPo 12S(4.3V/S)/42-52V; thrust per motor 4kg~5kg; recommended takeoff weight 19kgV62 280KV with FLUXER VTOL 18.1X7.2 propeller and MAD AMPX 80A (5-14S) ESC. |
| Total thrust loss allowance | 25%Coaxial configuration. |
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