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MAD V68 Pro IPE V1.0 230KV eVTOL Drone Motor, 12S, 13.9 kgf Max Thrust, AMPX 80A (5-14S)

MAD V68 Pro IPE V1.0 230KV eVTOL Drone Motor, 12S, 13.9 kgf Max Thrust, AMPX 80A (5-14S)

MAD

Regular price $268.50 USD
Regular price Sale price $268.50 USD
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Overview

MAD V68 Pro IPE V1.0 is a 230KV eVTOL drone motor designed for professional industrial eVTOL fixed-wing UAS in the 15–20 kg MTOW class. Stated thrust figures include 1.5–6.5 kg per rotor, with maximum thrust up to 13.9 kg (13.9 kgf) per rotor, and a recommended hover thrust of 5.0–7.0 kgf.

The motor is specified with IP35 protection and supports centrifugal heat dissipation. It is also described as being used with large-pitch eVTOL CF propellers, and the motor with propeller is designed to automatically return to a horizontal position relative to the wing upon shutdown.

Key Features

  • 230KV (Energy Efficient / Industry Professional Edition text shown)
  • Maximum thrust: 13.9 kg (13.9 kgf)
  • Efficiency: >80% (text shown)
  • Nominal voltage: 12S LiPo battery
  • Degree of protection: IP35
  • Centrifugal heat dissipation: YES
  • Recommended ESC: MAD AMPX 80A (5–14S)

Specifications

Motor model MAD V68 PRO IPE V1.0
KV 230KV
Number of pole pairs 14
Stator Anticorrosive
Varnished wire degree 150°C
Degree of protection IP35
Motor size D:72 × 43.5 mm
Motor weight 430 g (spec sheet); 378 g (also stated)
Internal resistance 30.5 mΩ
No load current 2.1 A / 20 V
Maximum current 85 A
Maximum power 3894 W
Maximum torque 3.78 Nm
Maximum thrust 13.9 kg (13.9 kgf)
Nominal voltage 12S LiPo battery
Motor balance 150°C
Motor balance ≤10 mg
Rotor balance ≤5 mg
Centrifugal heat dissipation YES
Cable length 80 mm 16# Awg(Black) silicone
Shaft diameter IN: 12 mm
Bearing 6801ZZ*2
Disruptive test 500 V
Recommended propellers 22x6.6, 22.1x7.4
Product boxed weight 600 g (110 x 110 x 55 mm)
Single rotor take-off weight 5 kg ~ 7 kg

Drawing Labels (Mounting / Dimensions)

  • Motor mounting holes: Ø25-M3x4, Ø30-M3x4
  • Propeller mounting holes: Ø12-M3x4, Ø18-M3x4, Ø22-M3x4
  • Additional drawing labels (mm): 37.5, 2, 4, Ø6, Ø48, Ø72
  • Also specified: Motor mounting holes D:25 M3×4, D:30 M4×4; Propeller mounting holes D:12 M3×4, 18 M3×4, 22 M3×4

Performance Data (Input 48 V, 25°C, Sea Level Text Shown)

Analytical Graph of Motor Operation legend (text shown): I = Current, P = Input Power, η = Electrical Efficiency, T = Thrust, N = Rotational Speed. The data is stated as measured with an input voltage of 48 V at 25°C and sea level; rotational speed adjusted by throttle.

Test Setup (Text Shown)

  • MAD V68 PRO IPE 230KV
  • Recommended ESC: AMPX 80A (5–14S)
  • Nominal voltage reference: 12S (MAX HOT text shown)
  • Propellers shown: FLUXER PRO 22x6.6 MATT; CF FLUXER 22.1x7.4 VTOL

FLUXER PRO 22x6.6 MATT (12S / MAX HOT Text Shown)

Throttle (%) Voltage (V) Current (A) Input Power (W) Output Power (W) Torque (N·m) RPM Thrust (gf) Efficiency (%) Efficiency (g/W)
30 48.23 4.25 205.0 134.2 0.436 2939 1814 65.5 8.9
35 48.18 5.89 283.8 197.3 0.559 3370 2352 69.5 8.3
40 48.1 8.32 400.2 300.5 0.746 3847 3116 75.1 7.8
45 48.01 11.34 544.4 423.9 0.938 4315 3912 77.9 7.2
50 47.92 14.48 693.9 553.7 1.115 4742 4683 79.8 6.7
55 47.82 17.8 851.2 684.4 1.281 5104 5235 80.4 6.1
60 47.69 21.95 1046.8 844.6 1.484 5435 5995 80.7 5.7
65 47.55 26.49 1259.6 1023.9 1.696 5765 6879 81.3 5.5
70 47.4 31.44 1490.3 1214.6 1.902 6098 7598 81.5 5.1
75 47.21 36.99 1746.3 1431.8 2.131 6416 8459 82 4.8
80 47.05 42.48 1998.7 1631.8 2.313 6734 9146 81.6 4.6
85 46.82 49.44 2314.8 1885.5 2.559 7036 10094 81.5 4.4
90 46.6 56.26 2621.7 2123.6 2.767 7329 11023 81 4.2
95 46.35 63.96 2964.5 2377.6 2.989 7596 11815 80.2 4.0
100 45.98 74.91 3444.4 2741.8 3.295 7946 12826 79.6 3.7

CF FLUXER 22.1x7.4 VTOL (12S / MAX HOT Text Shown)

Throttle (%) Voltage (V) Current (A) Input Power (W) Output Power (W) Torque (N·m) RPM Thrust (gf) Efficiency (%) Efficiency (g/W)
30 48.21 4.88 235.3 159.2 0.526 2890 2064 67.7 8.8
35 48.16 6.61 318.3 224.4 0.654 3277 2530 70.5 7.9
40 48.08 9.17 440.9 329.5 0.846 3719 3333 74.7 7.6
45 47.98 12.67 607.9 474.3 1.082 4186 4257 78 7.0
50 47.86 16.47 788.3 623.1 1.297 4588 5022 79 6.4
55 47.73 20.52 979.4 785.5 1.515 4951 5821 80.2 5.9
60 47.58 25.56 1216.1 973.7 1.762 5277 6683 80.1 5.5
65 47.41 31.01 1470.2 1179.6 2.014 5593 7745 80.2 5.3
70 47.25 35.89 1695.8 1353.3 2.196 5885 8409 79.8 5.0
75 47.07 41.82 1968.5 1573.1 2.421 6205 9138 79.9 4.6
80 46.84 48.94 2292.3 1827.6 2.694 6477 10205 79.7 4.5
85 46.6 56.22 2619.9 2083.9 2.939 6771 10932 79.5 4.2
90 46.33 64.19 2973.9 2342.9 3.188 7018 11993 78.8 4.0
95 46.02 73.61 3387.5 2638.2 3.472 7256 12939 77.9 3.8
100 45.62 85.35 3893.7 2995.7 3.771 7586 13908 76.9 3.6

Operating Notes (Text Shown)

The above data are stated as theoretical values at 48 V and for reference only. At 25°C with no additional cooling device: current over 85 A is stated as non-working zone; 31–85 A is stated as short-term working zone (about 10–30 s); below 31 A is stated as sustainable working zone. Control motor running time according to working environment temperature and heat dissipation conditions.

What’s Included

  • Motor x1
  • Propeller plate x1
  • 3.5 mm bullet connector x3
  • Heat shrinkable tube x3
  • M3*10 motor screws x4
  • M3*12 propeller screws x2
  • Sticker x2

Applications

  • Professional industrial eVTOL fixed-wing UAS (stated 15–20 kg MTOW)
  • Multi-rotor or VTOL propulsion where 12S-class testing data and 22-inch propeller setups are required

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

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