Overview
MAD X5225 (Long Shaft) IPE is an eVTOL airplane drone motor designed for efficiency-focused endurance flying and operation in harsh conditions. The available performance sheet is for a 225KV configuration on 12S LiPo (nominal), with propeller-dependent thrust and temperature limits.
Key Features
- 225KV configuration (as labeled on the performance sheet).
- Anticorrosive stator.
- Varnished wire degree: 220C.
- Degree of protection: IP35.
- Centrifugal heat dissipation: YES.
- Precision balance specs listed for rotor and motor (mg-level).
Specifications
Motor Data
| Motor model | MAD X5225 IPE V1.0 |
| KV | 225 KV |
| Number of pole pairs | 14 |
| Stator | Anticorrosive |
| Varnished wire degree | 220C |
| Motor balance (temperature) | 180C |
| Motor size | D:60 x 111 mm |
| Degree of protection | IP35 |
| Cable length | 100 mm, 14# AWG (black) silicone |
| Centrifugal heat dissipation | YES |
| Rotor balance | <= 5 mg |
| Motor balance (residual unbalance) | <= 10 mg |
| Propeller mounting | M8 nut |
| Shaft diameter | IN: 10 mm |
| Motor mounting holes | D:30 M4 x 4, D:44 M4 x 4 |
| Bearing | EZ0 6900ZZ x1; EZO 6800ZZ x2 |
| Disruptive test | 500 V |
Drawing and Mount Holes (as marked)
| Outer diameter | Ø60 |
| Overall length | 111 |
| Body length segments | 56, 55 |
| Front feature diameter | Ø14 |
| Shaft step diameter | Ø8 |
| Shaft lengths (marked) | 39.2, 27.5 |
| Thread | M8 x 1 |
| Front face holes | 8-M4 |
| Front face diameters (marked) | Ø44, Ø30 |
| Plate features (marked) | 4-Ø4.2, Ø74, Ø70, Ø44, 3.5, Ø8.1, 85, Ø19 |
Performance Sheet (12S)
| Nominal voltage | 12S LiPo battery |
| No load current | 2.45A / 20V |
| Internal resistance | 25 mΩ |
| Motor weight | 506 g |
| Maximum current | 68.3 A |
| Maximum power | 2877 W |
| Maximum torque | 2.73 Nm |
| Maximum thrust | 10.2 kg |
| Recommended ESC | MAD AMPX 80A (5-14S) |
| Recommended propellers | 19x10, 20x10 |
| Single rotor take-off weight | 3 kg ~ 4.5 kg |
| UAV take-off weight (12S-36V) | 18 kg (quadcopter); 27 kg (hexacopter); 36 kg (octocopter) |
| Max (temperature limit label) | 105C |
Test Data Table (12S, FALCON 19x10)
| Throttle (%) | Voltage (V) | Current (A) | Input Power (W) | Output Power (W) | Torque (Nm) | RPM | Thrust (gf) | Efficiency (gf/W) |
|---|---|---|---|---|---|---|---|---|
| 30 | 44.28 | 4.12 | 182.4 | 77.7 | 0.270 | 2749 | 1113 | 6.1 |
| 35 | 44.18 | 5.75 | 254.0 | 130.0 | 0.380 | 3268 | 1573 | 6.2 |
| 40 | 44.13 | 7.71 | 340.2 | 191.7 | 0.493 | 3714 | 2061 | 6.1 |
| 45 | 44.04 | 9.69 | 426.7 | 257.6 | 0.596 | 4128 | 2477 | 5.8 |
| 50 | 43.96 | 11.98 | 526.6 | 336.7 | 0.716 | 4490 | 2910 | 5.5 |
| 55 | 43.89 | 14.5 | 636.4 | 420.8 | 0.824 | 4877 | 3336 | 5.2 |
| 60 | 43.8 | 17.83 | 781.0 | 541.1 | 0.987 | 5235 | 4000 | 5.1 |
| 65 | 43.62 | 21.41 | 933.9 | 666.8 | 1.142 | 5576 | 4631 | 5.0 |
| 70 | 43.49 | 24.93 | 1084.2 | 792.1 | 1.276 | 5928 | 5143 | 4.7 |
| 75 | 43.32 | 29.57 | 1281.0 | 952.7 | 1.440 | 6318 | 5836 | 4.6 |
| 80 | 43.18 | 34.76 | 1500.9 | 1130.5 | 1.613 | 6693 | 6440 | 4.3 |
| 85 | 43 | 40.84 | 1756.1 | 1336.6 | 1.814 | 7036 | 7207 | 4.1 |
| 90 | 42.75 | 47.73 | 2040.5 | 1566.7 | 2.033 | 7359 | 7979 | 3.9 |
| 95 | 42.53 | 54.41 | 2314.1 | 1776.6 | 2.209 | 7680 | 8546 | 3.7 |
| 100 | 42.31 | 61.8 | 2614.8 | 1999.5 | 2.403 | 7946 | 8996 | 3.4 |
Max (label in table): 72C
Test Data Table (12S, FALCON 20x10)
| Throttle (%) | Voltage (V) | Current (A) | Input Power (W) | Output Power (W) | Torque (Nm) | RPM | Thrust (gf) | Efficiency (gf/W) |
|---|---|---|---|---|---|---|---|---|
| 30 | 44.3 | 4.2 | 186.1 | 92.9 | 0.322 | 2754 | 1288 | 6.9 |
| 35 | 44.22 | 5.99 | 264.9 | 151.4 | 0.442 | 3271 | 1757 | 6.6 |
| 40 | 44.16 | 8.07 | 356.4 | 222.0 | 0.571 | 3713 | 2255 | 6.3 |
| 45 | 44.05 | 10.25 | 451.5 | 297.3 | 0.693 | 4097 | 2722 | 6 |
| 50 | 43.96 | 12.98 | 570.6 | 395.1 | 0.846 | 4460 | 3254 | 5.7 |
| 55 | 43.88 | 16 | 702.1 | 499.6 | 0.991 | 4814 | 3820 | 5.4 |
| 60 | 43.74 | 19.61 | 857.7 | 624.1 | 1.151 | 5178 | 4457 | 5.2 |
| 65 | 43.61 | 23.4 | 1020.5 | 760.4 | 1.315 | 5522 | 5040 | 4.9 |
| 70 | 43.44 | 27.72 | 1204.2 | 910.8 | 1.490 | 5837 | 5716 | 4.7 |
| 75 | 43.27 | 32.89 | 1423.2 | 1088.5 | 1.672 | 6217 | 6329 | 4.4 |
| 80 | 43.07 | 39.2 | 1688.3 | 1305.2 | 1.902 | 6553 | 7273 | 4.3 |
| 85 | 42.89 | 45.21 | 1939.1 | 1499.9 | 2.077 | 6896 | 7933 | 4.1 |
| 90 | 42.66 | 52.36 | 2233.7 | 1724.3 | 2.285 | 7206 | 8758 | 3.9 |
| 95 | 42.41 | 60.26 | 2555.6 | 1966.6 | 2.504 | 7500 | 9465 | 3.7 |
| 100 | 42.13 | 68.29 | 2877.1 | 2213.9 | 2.730 | 7744 | 10211 | 3.5 |
Max (label in table): 97C
Test Notes (as stated on the sheet)
- Analytical graph legend: I = Current, P = Input Power, b7 = Electrical Efficiency, T = Thrust, N = Rotational Speed.
- Data measured with an input voltage of 48 V, at a temperature of 25C and sea level; rotational speed adjusted by the throttle.
- Values are theoretical and for reference only.
- With room temperature 25C and no additional cooling device: current over 68A is a non-working zone; 23-68A is a short-term (about 10-30s) working zone; below 23A is a sustainable working zone.
- Control motor running time according to working environment temperature and heat dissipation conditions.
For wiring, ESC matching, and integration questions, contact support at support@rcdrone.top or https://rcdrone.top/.
Whats Included
- Motor x1
- Propeller adapter x1
- M8 nut x1
- Prop plate x1
- Cross plate x1
- 4.0 mm bullet connector x3
- Heat shrinkable tube x3
- M4 x 12 motor screws x3
- M4 x 12 mm flat head machine screw x4
- M4 set screws x4
- Sticker x2
Applications
- eVTOL fixed-wing aircraft and endurance-focused UAV builds
- 12S multicopters (quadcopter/hexacopter/octocopter), based on the provided take-off weight guidance
Details

MAD X5225 long-shaft motor drawings provide key dimensions for mounting, including 111 mm overall length, an M8x1 shaft, and 4x M4 bolt holes.

The MAD X5225 motor package includes the propeller adapter, mounting plates, screws, heat-shrink, and 4.0mm bullet connectors for installation.

MAD X5225 225KV long-shaft motor includes a performance curve and key specs like 506 g weight, 10.2 kgf thrust, and 12S support for eVTOL builds.
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