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MAD M90C60 EEE 9KV Manned Drone Motor, 354-400V, 200.1 kgf Max Thrust, 12.7 kg

Original price was: $7,500.00.Current price is: $150.00.

SKU: BVHB1865366008 Category:

Description

Overview

MAD M90C60 EEE is a manned drone motor (9KV) designed for large manned multi-rotor aircraft, electric paragliders, large eVTOL UAVs, paramotors and paratrikes. It is positioned as an ultra-heavy-duty propulsion system for sustained high-load operation, supporting 70100 kg single-axis payloads for aerial mobility and cargo lift missions.

Key Features

  • KV rating: 9KV (EEE: Enthusiasts Extreme Edition)
  • Recommended hover thrust: 70100 kgf
  • Maximum thrust: 200.1 kgf (maximum thrust may depend on battery level, propeller type, air pressure, and other conditions)
  • Optimized weight: 12.7 kg
  • Efficiency: >90%
  • Power output (positioning): 45 kW
  • Maximum power (specification): 55.6 kW
  • Recommended propeller size: 72×31 (CB2 PROP 72×31 MATT referenced)
  • Recommended ESC (specification): SineSic Pro 160A 30KW (150V~435V)
  • Recommended FOC ESC/Prop system (positioning): HB110-72×31 drone arm set

Specifications

Motor Data

Motor Model MAD M90C60 EEE V1.0 Number of pole pairs 21
Stator TAIWAN / Anticorrosive Varnished wire degree 220C
Motor size D:257 x 123 mm Magnet degree 180C
Degree of protection Rain protection Cable length 250 mm (extended enameled wires)
Centrifugal heat dissipation Independent Rotor balance 20 mg
Propeller mounting holes D:75 M8x6 Motor balance 30 mg
Shaft diameter IN: 35 mm Motor mounting holes D:140 M8x6
Bearing 6007ZZ x2 (SKF listed) Disruptive test 1000 V

Electrical & System Specifications

RPM/V 9 KV Nominal voltage 354~400V
No load current 1.44A / 40V Internal resistance 40.5 m
Motor weight 12.7 kg Product boxed weight 14 kg
Maximum current 150.8 A Maximum power 55.6 kW
Maximum thrust 200.1 kg Maximum torque 178.9 Nm
Recommended ESC SineSic Pro 160A 30KW (150V~435V) Recommended propellers 72×31
UAV take-off weight 100S-72 in/360 kg – Quadcopter; 540 kg – Hexacopter; 720 kg – Octocopter Single rotor take-off weight 70 kg ~ 100 kg

Analytical Graph Notes (Measured Conditions)

  • Variables: I = Current, P = Input Power, = Electrical Efficiency, T = Thrust, N = Rotational Speed
  • Measured at: input voltage 400 V, temperature 25C, sea level (rotational speed adjusted by throttle)

Performance Table (CB2 PROP 72×31 MATT, SineSic Pro 160A 30KW)

Input 354 V

Throttle (%) Voltage (V) Current (A) Input Power (W) Output Power (W) Torque (Nm) RPM Thrust (gf) Efficiency (%) Efficiency (gf/W)
30 353.69 11.94 4223.1 3722.8 32.318 1100 38132 88.2 9.0
35 353.63 17.22 6089.5 5440.9 41.400 1255 50974 89.3 8.4
40 353.61 24.73 8744.8 7802.1 53.370 1396 65229 89.2 7.5
45 353.65 32.35 11440.6 10256.7 64.268 1524 77400 89.7 6.8
50 353.61 40.63 14367.2 12926.4 74.675 1653 88799 90.0 6.2
55 353.53 49.85 17623.5 15791.1 85.339 1767 104749 89.6 5.9
60 353.54 60.93 21541.2 19180.5 97.842 1872 118748 89.0 5.5
65 353.51 72.74 25714.3 22698.6 110.140 1968 134255 88.3 5.2
70 353.39 83.41 29476.3 25959.0 120.335 2060 144578 88.1 4.9
75 353.41 97.79 34560.0 29911.6 133.474 2140 158014 86.5 4.6
80 353.4 111.75 39492.4 33693.7 144.933 2220 170431 85.3 4.3
85 353.26 131.27 46372.4 38383.2 160.760 2280 183080 82.8 3.9
90 353.23 146.61 51787.1 42240.5 172.379 2340 194407 81.6 3.8
95 353.22 151.81 53622.3 43387.9 174.673 2372 194858 80.9 3.6
100 353.23 150.8 53267.1 42694.9 172.757 2360 192735 80.2 3.6

Input 400 V

Throttle (%) Voltage (V) Current (A) Input Power (W) Output Power (W) Torque (Nm) RPM Thrust (gf) Efficiency (%) Efficiency (gf/W)
30 399.37 10.28 4105.5 3584.5 30.949 1106 37713 87.3 9.2
35 399.39 15.8 6310.4 5576.2 42.633 1249 52294 88.4 8.3
40 399.41 21.56 8611.3 7678.8 52.564 1395 64712 89.2 7.5
45 399.31 28.46 11364.4 10159.0 63.489 1528 77799 89.4 6.8
50 399.31 37.5 14974.1 13419.4 77.570 1652 94009 89.6 6.3
55 399.32 45.22 18057.3 16177.6 87.329 1769 105734 89.6 5.9
60 399.29 54.85 21901.1 19348.8 98.648 1873 121243 88.3 5.5
65 399.19 64.82 25875.5 22714.3 110.836 1957 135071 87.8 5.2
70 399.24 72.99 29140.5 25427.1 118.329 2052 145502 87.3 5.0
75 399.16 86.31 34451.5 29741.9 133.528 2127 159487 86.3 4.6
80 399.14 98.38 39267.4 33115.0 143.350 2206 168537 84.3 4.3
85 399.06 111.66 44559.0 36852.4 154.892 2272 181329 82.7 4.1
90 399.04 125.57 50107.5 40936.6 166.489 2348 190526 81.7 3.8
95 398.9 133.75 53352.9 42354.6 171.380 2360 196373 79.4 3.7
100 398.6 139.51 55608.7 44598.2 178.955 2380 200164 80.2 3.6

Whats Included

  • Motor x1
  • Propeller plate x1
  • Locate pin x1
  • 8.0 mm bullet connector x3
  • Heat shrinkable tube x3
  • M6x25 motor screws x6
  • M8x90 propeller screws x6
  • M8x55 propeller screws x6
  • Sticker x2
  • Additional accessories list also includes: M8x30 mm motor screws x6

Applications

  • Electric manned aircraft and PAV systems
  • Heavy-lift VTOL and long-range aerial transport platforms
  • Advanced aerospace and eVTOL propulsion projects

For integration guidance, compatibility checks (ESC/prop/arm set), and after-sales support, contact [email protected] or visit https://rcdrone.top/.

Details

MAD M90C60 EEE motor drawings provide key outer dimensions and bolt-circle details to help plan mounting and clearance.

The MAD M90C60 motor package includes a propeller plate, locate pin, 8mm bullet connectors with heat-shrink, mounting screws, and stickers for a cleaner install.

MAD M90C60 EEE 9KV motor is rated for 400V with up to 200.1 kgf max thrust, and it lists 70100 kgf as the recommended thrust range.

MAD M90C60 EEE 9KV motor documentation includes dimension drawings plus thrust, RPM, current, and efficiency tables at 354V and 400V.

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