Product overview
The MAD M50C35 PRO EEE Manned Drone Motor is a propulsion component for large manned multirotors, eVTOL aircraft, UAVs and electric paraglider, paramotor and paratrike installations. Its design positioning covers 30–40 kg single-axis payloads and 57–63 inch carbon fiber propellers. Configuration choices comprise 34KV-24S, 40KV-24S and 9KV-100S, alongside a motor-plus-PT1000 temperature-sensor option. These are motor configurations; the recommended ESC, propeller and drone-arm combinations define integration choices without establishing that those components accompany every motor.
The motor occupies D:191 × 94 mm and uses an anticorrosive stator, an NSK 6818ZZCM bearing and independent centrifugal heat dissipation. Installation interfaces include D:80 M6×6 motor mounting holes, two propeller mounting patterns and 150 mm extended enameled wires. Protection is specified as rain protection. Performance figures include 30~45kg sustained thrust and 113.7kg maximum thrust, alongside a separate 92.6 kgf peak figure. Other differing specifications are 4200g and 4205g weight, and 24S,100S support alongside 12–24S suitability; no configuration relationship resolves these differences.
Specifications
| Specification | Value & conditions |
|---|---|
| Product identity | MAD M50C35 PRO EEE Manned Drone Motor |
| Sustained thrust | 30~45kg |
| Max thrust | 113.7kg |
| Support voltage | 24S,100S |
| Weight | 4200g |
| Motor model | MAD M50C35 EEE V2.0 |
| Number of pole pairs | 31 |
| Stator | Anticorrosive |
| Varnished wire temperature rating | 220°C |
| Motor size | D:191 × 94 mm |
| Magnet temperature rating | 180°C |
| Degree of protection | Rain protection |
| Cable length | 150 mm (extended enameled wires) |
| Centrifugal heat dissipation | Independent |
| Rotor balance | ≤20 mg |
| Propeller mounting holes | D:50 M6×6, D:32 M4×4 |
| Motor balance | ≤30 mg |
| Shaft diameter | IN: 25 mm |
| Motor mounting holes | D:80 M6×6 |
| Bearing | NSK 6818ZZCM |
| Disruptive test | 1000 V |
| Selectable configurations | 34KV-24S; 40KV-24S; 9KV-100S; Motor+PT1000 temperature sensor |
| Intended applications | Large manned multirotors, electric paragliders, large eVTOL aircraft, UAVs, paramotors and paratrikes |
| Design payload positioning | 30–40 kg single-axis payloads |
| Supported propellers | 57–63 inch carbon fiber propellers |
| Additional peak thrust specification | 92.6 kgf |
| Power output | 25 kW |
| Additional motor weight specification | 4205g |
| Additional voltage suitability specification | 12–24S |
| Recommended propulsion combinations | 34KV: AMPX 300A(12-24S) ESC with CB2 63X22" propeller. 40KV: AMPX 300A(12-24S) ESC with CB2 57X19 propeller, or AMPX 200A(12-24S) ESC with fluxer pro 60X20 propeller. 9KV: HB40 Drone Arm Set FOC combination.34KV, 40KV and 9KV motor configurations. |
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