Motor Data |
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| 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 | 150°C |
| Degree of Protection | IP35 | Cable Length | 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 |
| SOLUTION | ||
| VTOL Motor/KV | VTOL Prop | VTOL ESC |
| V62 210KV | Fluxer VTOL 22.1x7.4 | MAD AMPX 80A (5-14S) |
| VTOL Battery(Lipo)=/Voltage | VTOL Thrust Per Motor(kg) | The recommended takeoff weight |
| 12S(4.3V/S)/42-52V | 4kg~6kg | 20kg |
| Note.For a coaxial configuration, a total thrust loss of 25% should be considered. | ||
| SOLUTION 2 | ||
| VTOL Motor/KV | VTOL Prop | VTOL ESC |
| V62 280KV | FLUXER VTOL 18.1X7.2 | MAD AMPX 80A (5-14S) |
| VTOL Battery(Lipo)=/Voltage | VTOL Thrust Per Motor(kg) | The recommended takeoff weight |
| 12S(4.3V/S)/42-52V | 4kg~5kg | 19kg |
| Note.For a coaxial configuration, a total thrust loss of 25% should be considered. | ||
