• MAD X8025 KV190 brushless drone motor with front mounting bolt pattern and vented black housing
  • MAD X8025 190KV brushless drone motor front view with black housing and circular mounting hole pattern
  • Front view of MAD X8025 IPE V1.0 190KV eVTOL drone motor with finned black housing and 4-bolt mount
  • MAD X8025 190KV brushless drone motor with black finned housing, top mount plate and visible copper windings
  • MAD X8025 190KV brushless drone motor with ribbed black housing, copper windings, and front mounting hub
  • MAD X8025 drone motor with three bullet-connector leads, mounting plate, screws, and hardware accessories
1 6

MAD X8025 IPE V1.0 190KV eVTOL Airplane Drone Motor, IP35, 12S, 21.7kg Max Thrust

MAD X8025 IPE V1.0 190KV eVTOL Airplane Drone Motor, IP35, 12S, 21.7kg Max Thrust

MAD

$448.50 USD
$448.50 USD
Sale Sold out
Taxes included. Shipping calculated at checkout.
KV Option
  • PayPal
  • Visa
  • Mastercard
  • American Express
  • JCB
  • Discover
  • Diners Club
  • Google Pay
  • Apple Pay
View full details

Overview

The MAD X8025 is an eVTOL airplane drone motor (MAD X8025 IPE V1.0) with 190KV option data provided for 12S operation. It includes published motor construction data, mounting drawing dimensions, accessory list, and propeller test tables (23x10 / 24x10 / 25x10).

Key Features

  • 190KV motor option data provided (MAD X8025 IPE 190KV)
  • Anticorrosive stator
  • Centrifugal heat dissipation: YES
  • Degree of protection: IP35
  • Rotor balance: ≤20 mg

Specifications

Motor Data (MAD X8025 IPE V1.0)

Motor Model MAD X8025 IPE V1.0
Number of pole pairs 14
Stator Anticorrosive
Varnished wire Degree 220 C
Motor Size D:90 72.15 mm
Motor Balance 180 C
Degree of Protection IP35
Cable Length 100mm (extended Enameled wires)
Centrifugal Heat Dissipation YES
Rotor Balance ≤20 mg
Propeller Mounting Holes D:20 M3 4, M10 Nut
Motor Balance ≤30 mg
Shaft Diameter IN: 12 mm
Motor Mounting Holes D:45 M5 4
Bearing EZO 6900ZZ*3
Disruptive test 500 V

Published Specifications (MAD X8025 IPE 190KV, 12S)

RPM/V 190 KV
No Load Current 6.0A / 20V
Motor Weight 1016 g
Maximum Current 147 A
Maximum thrust 21.7 kg
Nominal Voltage 12S lipo battery
Internal resistance 80ma9
Maximum Power 6023 W
Maximum Torque 6.7 Nm
Recommended ESC MAD AMPX 150A (5-14S)
Recommended Propellers 23x10, 24x10, 25x10
Recommended battery thrust 6.5~9.0 kgf
Single rotor take-off weight 6.5kg ~ 9kg
UAV take-off weight 12S-25"/36kg-Quadcopter; 54kg-Hexacopter; 72kg-Octocopter

Prop Test Data (12S) b 23x10

Throttle (%) Voltage (V) Current (A) Input Power (W) Output Power (W) Torque (N b7m) RPM Thrust (gf) Efficiency (gf/W) MAX
30 43.87 6.79 297.9 148.7 0.577 2461 1894 6.4
35 43.85 9.44 413.9 227.7 0.764 2846 2520 6.1
40 43.71 12.83 560.8 348.6 1.018 3270 3402 6.1
45 43.74 17.15 750.1 498.3 1.297 3669 4338 5.8
50 43.52 21.54 937.4 659.6 1.561 4035 5280 5.6
55 43.46 26.82 1165.6 847.4 1.865 4339 6184 5.3
60 43.31 32.41 1403.7 1053.5 2.145 4690 7258 5.2 74 C
65 43.26 39.28 1699.3 1297.2 2.468 5019 8371 4.9
70 43.05 47.47 2043.6 1601.8 2.850 5367 9599 4.7
75 42.93 56.92 2443.6 1947.9 3.261 5704 10925 4.5
80 42.62 68.4 2915.2 2362.4 3.743 6027 12192 4.2
85 42.39 83.38 3534.5 2859.0 4.294 6358 13952 3.9
90 42.12 96.22 4052.8 3303.0 4.707 6701 15425 3.8
95 41.87 112.81 4723.4 3871.1 5.325 6942 16958 3.6
100 41.52 125.47 5209.5 4235.3 5.618 7199 18002 3.5

Prop Test Data (12S) b 24x10

Throttle (%) Voltage (V) Current (A) Input Power (W) Output Power (W) Torque (N b7m) RPM Thrust (gf) Efficiency (gf/W) MAX
30 43.96 7.74 340.3 180.0 0.702 2449 2089 6.1
35 43.78 10.52 460.6 281.9 0.955 2819 2887 6.3
40 43.76 14.49 634.1 416.2 1.235 3218 3809 6.0
45 43.60 19.22 838.0 592.4 1.570 3603 4904 5.9
50 43.55 24.42 1063.5 770.3 1.845 3987 6037 5.7
55 43.40 29.78 1292.5 964.3 2.142 4300 7075 5.5
60 43.32 36.93 1599.8 1216.2 2.503 4640 7974 5.0 83 C
65 43.09 45.12 1944.2 1519.6 2.918 4973 9269 4.8
70 42.96 55.3 2375.7 1897.5 3.433 5278 10659 4.5
75 42.65 66.54 2837.9 2292.5 3.910 5599 12255 4.3
80 42.47 79.34 3369.6 2723.6 4.395 5917 13788 4.1
85 42.12 94.61 3985.0 3217.1 4.902 6267 15430 3.9
90 41.86 111.11 4651.1 3699.8 5.413 6527 16998 3.7
95 41.52 125.8 5223.2 4182.3 5.875 6798 18615 3.5
100 41.23 141.99 5854.2 4671.2 6.356 7018 20207 3.3

Prop Test Data (12S) b 25x10

Throttle (%) Voltage (V) Current (A) Input Power (W) Output Power (W) Torque (N b7m) RPM Thrust (gf) Efficiency (gf/W) MAX
30 43.93 8.1 355.8 201.8 0.789 2443 2391 6.7
35 43.80 11.28 494.1 311.8 1.064 2797 3263 6.6
40 43.76 15.45 676.1 457.0 1.383 3157 4258 6.3
45 43.63 20.91 912.3 655.9 1.751 3577 5528 6.1
50 43.44 25.42 1104.2 834.8 2.096 3804 6614 6.0
55 43.28 31.62 1368.5 1051.0 2.401 4181 7793 5.7
60 43.25 42.38 1832.9 1424.2 2.968 4583 9225 5.0
65 42.98 52.42 2253.0 1786.6 3.490 4889 10703 4.8
70 42.89 61.08 2619.7 2093.2 3.835 5212 12024 4.6
75 42.61 73.59 3135.7 2524.2 4.365 5523 13450 4.3
80 42.35 86.03 3643.4 2936.6 4.827 5810 15177 4.2
85 41.95 100.47 4214.7 3392.8 5.281 6135 17061 4.0
90 41.62 115.84 4821.3 3852.2 5.795 6348 19016 3.9
95 41.29 129.77 5358.2 4281.2 6.175 6621 20361 3.8
100 40.98 146.98 6023.5 4782.5 6.672 6845 21733 3.6 103 C

Test Notes (from published sheet)

  • Maximum thrust may depend on battery level, propeller type, air pressure and other conditions.
  • The analytical graph notes: I = Current, P = Input Power, b7 = Electrical Efficiency, T = Thrust, N = Rotational Speed.
  • The data above was measured with an input voltage of 48 V, at a temperature of 25 C and sea level. The rotational speed was adjusted by the throttle.
  • The above data are the theoretical values when the input voltage is 48V, for reference only. In the case of room temperature without additional cooling device, the current over 147A is non-working zone. 52-147A is short-term (about 10-30s) working zone, and below 52A is sustainable working zone. In actual use, please control the motor running time according to the working environment temperature and heat dissipation conditions.

Drawing and Mount Holes

Motor mounting holes 845 - M5*4
Front face hole callouts 830 - M5*8; 820 - M3*4
Motor outer diameter callout 890
Side dimension callout 67.15
Prop adapter plate 830; 4-85.1; thread M10*1.5; length 50; 33
Additional adapter dimensions 810; 832; 3.0
Cross plate diameter callouts 8100; 896; 5.2; 830; 845; thickness 6

Whatbs Included

  • Motor x1
  • Propeller adapter x1
  • Prop Adapter x1
  • Cross Plate x1
  • 4.0mm Bullet Connector x3
  • Heat Shrinkable Tube x3
  • M5*12 Motor Screws x4
  • M5*25 Prop Adapter Screws x4
  • M3*16 Propeller Screw x4
  • M10 Nut x1
  • Sticker x2

Support

For integration and compatibility questions (ESC, propellers, and mounting), contact support@rcdrone.top or visit https://rcdrone.top/.

Details

MAD X8025 eVTOL Airplane Drone Motor

The MAD X8025 IPE V1.0 motor drawing details overall dimensions and the bolt-hole layout to help match frames, mounts, and prop adapters.

MAD X8025 eVTOL Airplane Drone Motor

The MAD X8025 IPE V1.0 motor kit includes a propeller adapter, cross plate, bullet connectors, heat-shrink tubing, mounting screws, and stickers for installation.

MAD X8025 eVTOL Airplane Drone Motor

The MAD X8025 IPE V1.0 190KV motor is rated for 12S setups and lists up to 21.7kgf max thrust with IP35 protection and a 1016g motor weight.

MAD X8025 eVTOL Airplane Drone Motor

MAD X8025 IPE 190KV motor test data lists 12S performance with 24x10 and 25x10 prop setups, including RPM, thrust, and current draw.

Related Collections