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MAD V68 IPE V1.0 230KV eVTOL Drone Motor, 13.9kgf Max Thrust, IP35, 12mm Shaft, 12S

MAD V68 IPE V1.0 230KV eVTOL Drone Motor, 13.9kgf Max Thrust, IP35, 12mm Shaft, 12S

MAD

Regular price $268.50 USD
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Overview

MAD V68 IPE V1.0 is a 230KV eVTOL drone motor designed to carry payloads of 5–6.5 kg per rotor, with maximum thrust up to 13.9 kg per rotor. Unit motor weight is 378 g. It is intended for 15–20 kg MTOW professional industrial eVTOL fixed-wing UAS and is commonly paired with large-pitch eVTOL CF propellers for high load, high efficiency, and reliable endurance flight operation.

Key Features

  • Recommended hover thrust: 5.0–7.0 kgf
  • Maximum thrust: 13.9 kgf
  • Optimized weight: 378 g
  • Efficiency: >80%
  • Anticorrosive stator
  • Centrifugal heat dissipation: YES
  • Protection rating: IP35

Specifications

Motor Data

Motor Model MAD V68 IPE V1.0
KV (RPM/V) 230KV
Number of pole pairs 14
Stator Anticorrosive
Varnished wire Degree 150°C
Motor Size D:72 × 39.5 mm
Degree of Protection IP35
Cable Length 80 mm 16# AWG (Black) silicone
Centrifugal Heat Dissipation YES
Rotor Balance ≤5 mg
Motor Balance ≤10 mg
Bearing 6801ZZ*2
Disruptive test 500 V
Shaft Diameter IN: 12 mm
Propeller Mounting Holes D:12 M3×4, 18 M3×4, 22 M3×4
Motor Mounting Holes D:25 M3×4, D:30 M4×4
Motor Balance (listed) 150°C

Additional Electrical / Performance Specs

Nominal Voltage 12S lipo battery
No Load Current 2.1 A / 20 V
Internal resistance 30.5 mΩ
Motor Weight 378 g
Product Boxed Weight 548 g (110 x 110 x 55 mm)
Maximum Current 85 A
Maximum Power 3894 W
Maximum Torque 3.78 Nm
Maximum thrust 13.9 kg
Recommended Propellers 22x6.6, 22.1x7.4
Recommended ESC MAD AMPX 80A (5-14S)
Single rotor take-off weight 5 kg ~ 7 kg

Drawing Dimensions (as labeled)

Labeled dimensions Ø72, 37.5, 2, Ø48, Ø4
Motor mounting hole patterns (labeled) Ø30-M4×4; Ø25-M3×4
Propeller mounting hole patterns (labeled) Ø22-M3×4; Ø18-M3×4; Ø12-M3×4

Analytical Graph of Motor Operation (test conditions)

  • 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.
  • Legend: I = Current, P = Input Power, η = Electrical Efficiency, T = Thrust, N = Rotational Speed

Operation Data (MAD V68 IPE 230KV + FLUXER PRO 22x6.6 MATT + AMPX 80A (5-14S), 12S)

Throttle (%) Voltage (V) Current (A) Input Power (W) Output Power (W) Torque (N·m) RPM Thrust (gf) Efficiency (%) Efficiency (gf/W)
30 48.23 4.25 205.0 134.2 0.436 2939 1814 65.5 8.9
35 48.18 5.89 283.8 197.2 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 17.8 851.2 684.7 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 1631.6 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 2.889 7596 11815 80.2 4.0
100 45.98 74.91 3444.4 2741.8 3.295 7946 12826 79.6 3.7

Operation Data (MAD V68 IPE 230KV + CF FLUXER 22.1x7.4 VTOL + AMPX 80A (5-14S), 12S)

Throttle (%) Voltage (V) Current (A) Input Power (W) Output Power (W) Torque (N·m) RPM Thrust (gf) Efficiency (%) Efficiency (gf/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 1827.3 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

The above operation data are theoretical values when the input voltage is 48 V, for reference only. Under room temperature of 25°C and without additional cooling, current over 85 A is a non-working zone; 31–85 A is a short-term (about 10–30 s) working zone; and below 31 A is a sustainable working zone. Motor running time should be controlled based on ambient temperature and heat dissipation conditions.

For product selection and integration support, contact support@rcdrone.top or visit https://rcdrone.top/.

What’s Included

  • Motor x1
  • Propeller Plate x1
  • Prop Adapter x1
  • Ø4–6 Adapter Ring x1
  • 8.0 mm Bullet Connector x3
  • Heat Shrinkable Tube x3
  • M3*10 Motor Screws x4
  • M3*6 Prop Adapter Screws x4
  • M4*10 Motor Screws x4
  • M3*12 Propeller Screws x2
  • Sticker x2

Solution

VTOL Motor/KV VTOL Prop VTOL ESC
V68 230KV FLuxer VTOL 22x6.6 / 22.1x7.4 MAD AMPX 80A (5-14S)
VTOL Battery (Lipo) / Voltage VTOL Thrust Per Motor (kg) Recommended takeoff weight (4 rotors)
12S (4.3 V/S) / 42–52 V 5 kg ~ 7 kg 23 kg

Note: For a coaxial configuration, a total thrust loss of 25% should be considered.

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