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COMPONENT

V122 eVTOL Drone Motor

By MAD Components ↗

The MAD V122 eVTOL Drone Motor is a 1600g propulsion component available in 45KV and 90KV versions. Designed for 16–20kg payloads per rotor with a 42-inch carbon propeller, it provides defined motor and propeller mounting interfaces and centrifugal heat dissipation. A 25% total thrust loss should be considered for coaxial configurations.

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MAD Components V122 eVTOL drone motor, 45KV variant, shown at an angle
MAD Components V122 eVTOL drone motor, 45KV variant, shown at an angle
Motor modelMAD V122 IPE V2.0
Number of pole pairs19
StatorAnticorrosive
Varnished wire temperature rating220°C
Motor sizeD:145 × 53 mm
Magnet temperature rating180°C

Product overview

The MAD V122 eVTOL Drone Motor is a propulsion component for professional UAVs, identified as MAD V122 IPE V2.0 and offered in 45KV and 90KV versions. It is designed to carry payloads of 16–20kg per rotor with a 42-inch carbon propeller, while maximum thrust reaches up to 48kg per rotor. The motor weighs 1600g and measures D:145 × 53 mm. Its construction combines an anticorrosive stator, 19 pole pairs, two 6904ZZ bearings and centrifugal heat dissipation, with IP35 protection.

Integration interfaces include D:24 M4×4 and D:30 M5×4 propeller mounting patterns, D:50 M6×4 motor mounting holes, a shaft diameter specified as IN: 20 mm, and 150 mm extended enameled wires. The associated 45KV accessory configuration pairs Fluxer VTOL 40x13.1/42x14 propellers with a MAD AMPX 120A(12-24S) ESC and 24S(4.3V/S)/84-52V LiPo supply. For this configuration, thrust is 16kg ~ 20kg per motor and recommended four-rotor takeoff weight is 76kg. A 25% total thrust loss should be considered for coaxial configurations.

Specifications

SpecificationValue & conditions
Motor modelMAD V122 IPE V2.0
Number of pole pairs19
StatorAnticorrosive
Varnished wire temperature rating220°C
Motor sizeD:145 × 53 mm
Magnet temperature rating180°C
Degree of protectionIP35
Cable length150 mmExtended enameled wires.
Centrifugal heat dissipationYES
Rotor balance≤10 mg
Propeller mounting holesD:24 M4×4, D:30 M5×4
Motor balance≤20 mg
Shaft diameterIN: 20 mm
Motor mounting holesD:50 M6×4
Bearings6904ZZ*2
Disruptive test voltage500 V
KV options45KV; 90KV
Designed payload per rotor16-20kg per rotorWith a 42″ carbon propeller.
Maximum thrust per rotorUp to 48kg(105.8bl) per rotor
Unit motor weight1600g
Associated VTOL propellersFluxer VTOL 40x13.1/42x14Accessory configuration using MAD V122 IPE 45KV.
Associated VTOL ESCMAD AMPX 120A(12-24S)Accessory configuration using MAD V122 IPE 45KV.
Battery and voltage24S(4.3V/S)/84-52VVTOL accessory configuration using MAD V122 IPE 45KV, Fluxer VTOL 40x13.1/42x14 propellers and MAD AMPX 120A(12-24S) ESC; LiPo supply.
VTOL thrust per motor16kg ~ 20kgVTOL accessory configuration using MAD V122 IPE 45KV, Fluxer VTOL 40x13.1/42x14 propellers, MAD AMPX 120A(12-24S) ESC and 24S(4.3V/S)/84-52V LiPo supply.
Recommended takeoff weight76kgFour rotors using the MAD V122 IPE 45KV accessory configuration with Fluxer VTOL 40x13.1/42x14 propellers, MAD AMPX 120A(12-24S) ESC and 24S(4.3V/S)/84-52V LiPo supply.
Advisory total thrust loss allowance25% total thrust loss should be consideredCoaxial configuration.
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