MAD V185 IPE V1.0 60KV eVTOL Airplane Drone Motor, IP35, 21 Pole Pairs, 120.5 x 105 mm
MAD V185 IPE V1.0 60KV eVTOL Airplane Drone Motor, IP35, 21 Pole Pairs, 120.5 x 105 mm
MAD
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Overview
MAD V185 IPE is an eVTOL airplane drone motor designed for VTOL propulsion setups. This listing covers the MAD V185 IPE V1.0 motor, including mounting/drawing dimensions and a reference configuration for a 24S system.
Key Features
- KV rating: 60KV (V185 IPE 60KV)
- Anticorrosive stator
- Centrifugal heat dissipation: YES
- Ingress protection: IP35
- Balance specs: rotor balance 20 mg; motor balance 30 mg
For integration and compatibility questions (prop/ESC/battery matching and mounting), contact support@rcdrone.top or visit https://rcdrone.top/.
Specifications
| Motor model | MAD V185 IPE V1.0 |
| KV (RPM/V) | 60 KV |
| Number of pole pairs | 21 |
| Stator | Anticorrosive |
| Varnished wire temperature rating | 220C |
| Magnet temperature rating | 180C |
| Motor size | D: 120.5 x 105 mm |
| Degree of protection | IP35 |
| Cable length | 150 mm (extended enameled wires) |
| Bearings | EZO 6804ZZ*4; NSK 6814ZZ*1 |
| Disruptive test | 1000 V |
| No-load current | 5.1 A / 30 V |
| Internal resistance | 15 m |
| Motor weight | 3000 g |
| Maximum current | 305.3 A |
| Maximum power | 21160 W |
| Maximum torque | 50.7 Nm |
| Maximum thrust | 82.6 kg (also shown as 82.6 kgf) |
| Recommended hover thrust | 25 to 35 kgf |
| Efficiency | >80% |
| Nominal voltage | 24S LiPo battery |
| Recommended ESC | MAD AMPX 300A (12-24S) |
| Recommended propellers | 45 x 17.5 |
| Single-rotor take-off weight | 25 kg to 35 kg |
| Reference system label | 24S; MAX 96C |
Propeller / Mounting Interface (from motor data)
| Propeller mounting holes | D:34, M5 x 6 |
| Motor mounting holes | D:40, M5 x 8; D:60, M5 x 8 |
| Shaft diameter | IN: 20 mm |
Operating Data Table (96 V reference)
| Throttle (%) | Voltage (V) | Current (A) | Input Power (W) | Output Power (W) | Torque (N*m) | RPM | Thrust (gf) | Efficiency (%) | Efficiency (gf/W) |
|---|---|---|---|---|---|---|---|---|---|
| 30 | 98.24 | 14.06 | 1381.3 | 1004.3 | 6.272 | 1529 | 10971 | 72.7 | 7.9 |
| 35 | 98.05 | 19.98 | 1959.0 | 1495.0 | 8.252 | 1730 | 14350 | 76.3 | 7.3 |
| 40 | 97.97 | 27.99 | 2742.2 | 2165.9 | 10.504 | 1969 | 18220 | 79 | 6.6 |
| 45 | 97.66 | 40.83 | 3987.5 | 3232.9 | 13.869 | 2226 | 23688 | 81.1 | 5.9 |
| 50 | 97.49 | 53.81 | 5245.9 | 4262.6 | 16.621 | 2449 | 28308 | 81.3 | 5.4 |
| 55 | 97.21 | 67.52 | 6563.6 | 5378.4 | 19.403 | 2647 | 33770 | 81.9 | 5.1 |
| 60 | 96.98 | 84.8 | 8223.9 | 6729.1 | 22.706 | 2830 | 38566 | 81.8 | 4.7 |
| 65 | 96.71 | 101.09 | 9776.4 | 8017.9 | 25.573 | 2994 | 42709 | 82 | 4.4 |
| 70 | 96.53 | 123.04 | 11877.1 | 9544.6 | 28.843 | 3160 | 44773 | 80.4 | 3.8 |
| 75 | 96.12 | 147.24 | 14152.7 | 11353.3 | 32.616 | 3324 | 55471 | 80.2 | 3.9 |
| 80 | 95.8 | 173.48 | 16619.4 | 13192.8 | 36.181 | 3482 | 61936 | 79.4 | 3.7 |
| 85 | 95.34 | 202.6 | 19315.9 | 15123.2 | 39.762 | 3632 | 67124 | 78.3 | 3.5 |
| 90 | 94.98 | 232 | 22035.4 | 16985.1 | 43.160 | 3758 | 72221 | 77.1 | 3.3 |
| 95 | 94.48 | 263.57 | 24902.1 | 18933.3 | 46.514 | 3887 | 75435 | 76 | 3.0 |
| 100 | 92.75 | 305.31 | 28410.3 | 21160.9 | 50.670 | 3988 | 82602 | 74.5 | 2.9 |
I = Current, P = Input Power, = Electrical Efficiency, T = Thrust, N = Rotational Speed. Data measured with input voltage of 96 V at 25C and sea level; rotational speed adjusted by throttle.
The above data are theoretical values when the input voltage is 96 V (for reference only). In the case of room temperature of 25C and no additional cooling device: current over 305 A is a non-working zone; 101-305 A is a short-term (about 10-30 s) working zone; below 101 A is a sustainable working zone. Control motor running time based on working environment temperature and heat dissipation conditions.
Drawing and Mount Holes
- Overall diameter shown: 120.5
- Length shown: 101; additional segment shown: 4
- Diameters shown: 70 and 45
- Propeller pattern: 34 - M5*6; center bore: 11
- Mounting patterns shown: 60 and 40; note: 16 - M5 20 mm
- Additional drawing notes: cable exit location marked; 34; 6 - 5.1 (+0.05/0); 50; 34; 6; 11 (+0.03/-0.01); 6 - 10; 0.5; 30
Recommended Solution (Reference)
| VTOL motor / KV | MAD V185 IPE 60KV |
| VTOL prop | Fluxer VTOL 45 x 17.5 |
| VTOL ESC | MAD AMPX 300A (12-24S) |
| VTOL battery (LiPo) / voltage | 24S (4.3 V/S) / 84-104 V |
| VTOL thrust per motor | 25 kg to 35 kg |
| Recommended takeoff weight (4 rotors) | 120 kg |
Note: For a coaxial configuration, a total thrust loss of 25% should be considered.
Details
MAD V185 IPE V1.0 60KV eVTOL motor uses an M5 x6 mounting pattern and a 101 mm overall length for fit and installation planning.
MAD V185 IPE V1.0 60KV motor documentation includes performance curves and a 24S data table to help match props and power setups.
