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MAD X5225 Long Shaft IPE 225KV eVTOL Airplane Drone Motor IP35, 12S LiPo, 60x111mm, 10.2kgf, 2877W

MAD X5225 Long Shaft IPE 225KV eVTOL Airplane Drone Motor IP35, 12S LiPo, 60x111mm, 10.2kgf, 2877W

MAD

Regular price $219.00 USD
Regular price Sale price $219.00 USD
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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