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MAD M50C35 PRO EEE Manned Drone Motor (9KV/34KV/40KV) 24S/100S Heavy-Lift Propulsion

MAD M50C35 PRO EEE Manned Drone Motor (9KV/34KV/40KV) 24S/100S Heavy-Lift Propulsion

MAD

$1,798.50 USD
$1,798.50 USD
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Overview

The MAD M50C35 PRO EEE is a manned drone motor for large multirotor platforms, electric paraglider / paramotor systems, and large e-VTOL aircraft. It supports 57–63 inch carbon fiber propellers and is positioned for high-power, heavy-lift propulsion.

Sustained thrust 30~45 kg
Max thrust 113.7 kg
Support voltage 24S, 100S
Weight 4200 g

Key Features

  • Recommended hover thrust (variant-dependent): 30~40 kgf (9KV), 35~45 kgf (34KV), 30~40 kgf (40KV)
  • Maximum thrust (variant-dependent): 92.6 kgf (9KV), 113.7 kgf (34KV), 90.9 kgf (40KV)
  • Efficiency (variant-dependent): >78% (9KV), >83% (34KV), >82% (40KV)
  • Power output (provided description): 25 kW
  • Industrial-grade component positioning (provided description)

Specifications

Motor Data (Common)

Motor model MAD M50C35 EEE V2.0
Number of pole pairs 31
Stator Anticorrosive
Varnished wire degree 220°C
Motor size D:191 × 94 mm
Magnet degree 180°C
Degree of protection Rain protection
Cable length 150 mm (extended enameled wires)
Centrifugal heat dissipation Independent
Rotor balance ≤20 mg
Motor balance ≤30 mg
Propeller mounting holes D:50 M6×6, D:32 M4×4
Motor mounting holes D:80 M6×6
Shaft diameter IN: 25 mm
Bearing NSK 6818ZZCM
Disruptive test 1000 V

Drawing & Mounting (Extracted)

Outer diameter Ø191
Body width 83 + 11 (total 94)
Center feature diameter Ø90
Motor mounting pattern Ø80-M6×6
Prop mounting patterns Ø50-M6×6; Ø32-M4×4
Center bore Ø25
Center feature length 22
Hole callout Ø50-Ø6.2×6
Plate thickness callout 4

Variant: 9KV

  • Label: M50C35 Energy Efficient 9KV (Enthusiasts Extreme Edition)
  • Recommended hover thrust: 30~40 kgf
  • Maximum thrust: 92.6 kgf
  • Optimized weight: 4200 g
  • Efficiency: >78%
  • Test line label: MAD M50C35 EEE 9KV; FLUXER PRO 63x22 GLOSSY; FOC IGBT 60A (80~440V); 400V; MAX 126°C
RPM/V 9 KV
No load current 0.92A/30V
Motor weight 4200 g
Maximum current 49.1 A
Maximum thrust 92.6 kg
Recommended ESC FOC IGBT 60A (80-440V)
Recommended propellers 63x22
Nominal voltage 100S lipo battery
Internal resistance 58.8 mΩ
Product boxed weight 5750 g (330 x 265 x 135 mm)
Maximum power 19494 W
Maximum torque 63.9 Nm
UAV take-off weight 245-637 / 140 kg - Quadcopter; 210 kg - Hexacopter; 280 kg - Octocopter
Single rotor take-off weight 30 kg ~ 40 kg
Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [N·m] RPM Thrust [kgf] Efficiency [%] Efficiency [kgf/W]
30 398 2.74 1090.0 696.7 7.930 839 11 63.92 10.5
35 398 3.7 1472.0 1117.6 10.880 981 16 75.93 10.7
40 398 5.85 2328.0 1730.3 14.820 1115 21 74.33 8.8
45 398 8.09 3219.0 2360.2 18.090 1246 26 73.32 8.0
50 398 10.23 4071.0 3107.0 21.690 1368 31 76.32 7.7
55 398 12.7 5052.0 3993.6 25.700 1484 37 79.05 7.3
60 398 15.38 6114.0 4991.2 29.810 1599 43 81.64 7.1
65 398 18.79 7471.0 6168.2 34.590 1703 48 82.56 6.5
70 398 22.56 8968.0 7369.9 38.950 1807 56 82.18 6.2
75 397 25.18 9986.0 8364.9 42.200 1893 59 83.77 5.9
80 397 29.22 11586.0 10498.4 49.930 2008 68 90.61 5.8
85 397 34.95 13861.0 11991.3 54.480 2102 75 86.51 5.4
90 396 40.04 15868.0 13572.0 59.130 2192 81 85.53 5.1
95 397 48.14 19102.0 15072.8 63.440 2269 89 78.91 4.6
100 397 49.14 19494.0 15334.1 63.920 2291 93 78.66 4.8

Note (9KV sheet): Data are theoretical values when the input voltage is 400 V. For room temperature of 25°C and no additional cooling device, the current over 49 A is non-working zone, 15–49 A is short-term (about 10–30 s) working zone, and below 15 A is sustainable working zone. Control running time according to working environment temperature and heat dissipation conditions.

Variant: 34KV

  • Label: M50C35 Energy Efficient 34KV (Enthusiasts Extreme Edition)
  • Recommended hover thrust: 35~45 kgf
  • Maximum thrust: 113.7 kgf
  • Optimized weight: 4205 g
  • Efficiency: >83%
  • Test line label: MAD M50C35 EEE 34KV; FLUXER PRO 63x22 GLOSSY; AMPX 300A (12-24S); 24S
RPM/V 34 KV
No load current 3.7A/30V
Motor weight 4205 g
Maximum current 251.5 A
Maximum thrust 113.7 kg
Recommended ESC MAD AMPX 300A (12-24S)
Recommended propellers 63x22
Nominal voltage 24S lipo battery
Internal resistance 14.7 mΩ
Product boxed weight 5755 g (330 x 265 x 135 mm)
Maximum power 24987 W
Maximum torque 78.4 Nm
UAV take-off weight 245-637 / 160 kg - Quadcopter; 240 kg - Hexacopter; 320 kg - Octocopter
Single rotor take-off weight 35 kg ~ 45 kg
Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [N·m] RPM Thrust [gf] Efficiency [%] Efficiency [gf/W]
30 100.6 10.63 1069.4 855.5 8.841 924 13360 80.00 12.5
35 100.54 15.2 1528.2 1246.2 11.259 1057 17031 81.50 11.1
40 100.78 21.82 2199.0 1775.0 14.232 1191 22773 80.70 10.4
45 100.61 30.57 3075.6 2511.5 17.858 1343 28863 81.70 9.4
50 100.46 42 4219.3 3534.7 22.608 1493 35262 83.80 8.4
55 100.58 54.55 5486.6 4706.2 27.554 1631 42642 85.80 7.8
60 100.56 68.22 6860.2 5919.3 32.374 1746 49381 86.30 7.2
65 100.52 83.9 8433.6 7198.8 36.761 1870 56551 85.40 6.7
70 100.4 102.19 10259.9 8889.7 42.723 1987 63961 86.60 6.2
75 100.27 122.51 12284.1 10566.1 48.070 2099 72525 86.00 5.9
80 100.2 147.52 14781.5 12591.8 54.532 2205 80002 85.20 5.4
85 100.08 171.25 17138.7 14472.0 59.414 2326 87814 84.40 5.1
90 99.9 203.99 20378.6 16845.9 66.584 2416 96733 82.70 4.7
95 99.58 232.09 23111.5 18677.9 71.430 2497 106740 80.80 4.6
100 99.36 251.48 24987.1 20739.3 78.409 2526 113654 83.00 4.5

Variant: 40KV

  • Label: M50C35 Energy Efficient 40KV (Enthusiasts Extreme Edition)
  • Recommended hover thrust: 30~40 kgf
  • Maximum thrust: 90.9 kgf
  • Optimized weight: 4177 g
  • Efficiency: >82%
  • Test line label: MAD M50C35 EEE 40KV; CB2 PROP 60x20 MATT; AMPX 300A (12-24S); 24S; MAX 138°C
RPM/V 40 KV
No load current 3.6A/20V
Motor weight 4177 g
Maximum current 216.6 A
Maximum thrust 90.9 kg
Recommended ESC MAD AMPX 300A (12-24S)
Recommended propellers 57x19, 60x20
Nominal voltage 24S lipo battery
Internal resistance 10 mΩ
Product boxed weight 5727 g (330 x 265 x 135 mm)
Maximum power 20967 W
Maximum torque 52.1 Nm
UAV take-off weight 245-607 / 140 kg - Quadcopter; 210 kg - Hexacopter; 280 kg - Octocopter
Single rotor take-off weight 30 kg ~ 40 kg

40KV Performance Table (CB2 PROP 57x19 MATT, MAX 130°C)

Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [N·m] RPM Thrust Efficiency [%] Efficiency
30 98.66 12.3 1213.5 910.8 8.091 1075 12865 75.10 10.6
35 98.68 18.03 1779.2 1361.3 10.569 1230 16662 76.50 9.4
40 98.54 25.34 2497.0 1991.0 13.688 1389 21496 79.70 8.6
45 98.53 36.78 3623.9 2921.9 17.637 1582 27746 80.60 7.7
50 98.37 49.01 4821.1 3998.3 21.830 1749 34236 82.90 7.1
55 98.3 63.68 6259.7 5276.9 26.482 1903 40549 84.30 6.5
60 98.17 77.5 7608.2 6398.5 29.851 2047 46604 84.10 6.1
65 98.17 98.03 9623.6 7949.1 34.791 2182 53790 82.60 5.6
70 98.01 118.31 11595.6 9438.8 38.938 2315 61280 81.40 5.3
75 97.92 140.81 13788.1 11195.9 43.606 2452 68220 81.20 4.9
80 97.94 164.23 16084.7 12996.4 48.407 2564 74006 80.80 4.6
85 97.83 195.21 19097.4 15201.5 54.069 2685 81462 79.60 4.3
90 98.12 229.66 22534.2 17847.1 60.871 2800 85765 79.20 3.8

40KV Performance Table (CB2 PROP 60x20 MATT, MAX 138°C)

Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [N·m] RPM Thrust Efficiency [%] Efficiency
30 98.47 12.4 1221.0 895.0 7.117 1201 14430 73.30 11.8
35 98.46 19.2 1890.4 1414.0 10.040 1345 18964 74.80 10.0
40 98.33 26.8 2635.2 1976.4 12.592 1499 22645 75.00 8.6
45 98.33 35.8 3520.2 2678.9 15.571 1643 27640 76.10 7.9
50 98.43 47.4 4665.6 3601.8 19.270 1785 33945 77.20 7.3
55 98.35 59.8 5881.3 4593.3 23.075 1901 39362 78.10 6.7
60 98.26 73.1 7182.8 5753.4 31.419 2024 45693 80.10 6.4
65 98.43 86.5 8514.2 6777.3 32.284 2123 51637 79.60 6.1
70 98.42 100.8 9920.7 7847.3 33.471 2239 56700 79.10 5.7
75 98.49 118.4 11661.2 9200.7 37.012 2374 62129 78.90 5.3
80 98.47 131 12899.6 10100.4 39.211 2460 67134 78.30 5.2
85 98.37 148.6 14617.8 11416.5 42.112 2589 72374 78.30 5.2
90 98.56 169.7 16386.2 12699.3 44.935 2699 78315 77.50 4.8
95 97.35 193 18788.6 14523.5 48.976 2832 86010 77.30 4.6
100 96.8 216.6 20966.9 16102.6 52.129 2950 90980 76.80 4.3

Recommended Configurations

  • 34KV: ESC AMPX 300A (12-24S); Propeller CB2 63x22
  • 40KV: ESC AMPX 300A (12-24S); Propeller CB2 57x19; or ESC AMPX 200A (12-24S); Propeller Fluxer Pro 60x20
  • 9KV: FOC combo HB40 Drone Arm Set

What’s Included

  • Motor x1
  • Propeller Plate x1
  • Locate Pin x1
  • 8.0mm Bullet Connector x3
  • Heat Shrinkable Tube x3
  • M6*25 Motor Screws x6
  • M6*45 Prop Adapter Screws x6
  • M6*60 Propeller Screws x6
  • Sticker x2

Applications

  • Manned drones and hybrid VTOL platforms
  • Electric air mobility (EAM) applications
  • Large multirotor propulsion for ultra-heavy configurations
  • Electric paraglider / paramotor / para-trike propulsion systems

For compatibility checks (ESC, propeller, voltage system) and integration support, contact support@rcdrone.top or visit https://rcdrone.top/.

Details

MAD M50C35 PRO EEE Manned Drone Motor

The dimensioned motor drawings provide key outer size and mounting-hole layout details to help with frame fitment and installation.

MAD M50C35 PRO EEE Manned Drone Motor

The MAD M50C35 PRO EEE motor package includes a propeller plate, locate pin, 8.0mm bullet connectors, heat-shrink tubing, and mounting screws for installation.

MAD M50C35 PRO EEE Manned Drone Motor

The MAD M50C35 Pro EEE manned-drone motor datasheet lists a 400V system rating and a 30–40 kgf thrust range for build planning.

MAD M50C35 PRO EEE Manned Drone Motor

The MAD M50C35 PRO 34KV motor is rated for 24S setups, with a listed 35–45 kgf thrust range, 4205 g weight, and >83% efficiency.

MAD M50C35 PRO EEE Manned Drone Motor

MAD M50C35 PRO EEE is a 24S, 40kV manned drone motor with published thrust curves and efficiency data for build planning.

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