Overview

MAD V185 IPE is an eVTOL airplane drone motor designed for VTOL propulsion setups. This listing covers the MAD V185 IPE V1.0 motor, including mounting/drawing dimensions and a reference configuration for a 24S system.

Key Features

KV rating: 60KV (V185 IPE 60KV)
Anticorrosive stator
Centrifugal heat dissipation: YES
Ingress protection: IP35
Balance specs: rotor balance 20 mg; motor balance 30 mg

For integration and compatibility questions (prop/ESC/battery matching and mounting), contact [email protected] or visit https://rcdrone.top/.

Specifications

Motor model	MAD V185 IPE V1.0
KV (RPM/V)	60 KV
Number of pole pairs	21
Stator	Anticorrosive
Varnished wire temperature rating	220C
Magnet temperature rating	180C
Motor size	D: 120.5 x 105 mm
Degree of protection	IP35
Cable length	150 mm (extended enameled wires)
Bearings	EZO 6804ZZ4; NSK 6814ZZ1
Disruptive test	1000 V
No-load current	5.1 A / 30 V
Internal resistance	15 m
Motor weight	3000 g
Maximum current	305.3 A
Maximum power	21160 W
Maximum torque	50.7 Nm
Maximum thrust	82.6 kg (also shown as 82.6 kgf)
Recommended hover thrust	25 to 35 kgf
Efficiency	>80%
Nominal voltage	24S LiPo battery
Recommended ESC	MAD AMPX 300A (12-24S)
Recommended propellers	45 x 17.5
Single-rotor take-off weight	25 kg to 35 kg
Reference system label	24S; MAX 96C

Propeller / Mounting Interface (from motor data)

Propeller mounting holes	D:34, M5 x 6
Motor mounting holes	D:40, M5 x 8; D:60, M5 x 8
Shaft diameter	IN: 20 mm

Operating Data Table (96 V reference)

Throttle (%)	Voltage (V)	Current (A)	Input Power (W)	Output Power (W)	Torque (N*m)	RPM	Thrust (gf)	Efficiency (%)	Efficiency (gf/W)
30	98.24	14.06	1381.3	1004.3	6.272	1529	10971	72.7	7.9
35	98.05	19.98	1959.0	1495.0	8.252	1730	14350	76.3	7.3
40	97.97	27.99	2742.2	2165.9	10.504	1969	18220	79	6.6
45	97.66	40.83	3987.5	3232.9	13.869	2226	23688	81.1	5.9
50	97.49	53.81	5245.9	4262.6	16.621	2449	28308	81.3	5.4
55	97.21	67.52	6563.6	5378.4	19.403	2647	33770	81.9	5.1
60	96.98	84.8	8223.9	6729.1	22.706	2830	38566	81.8	4.7
65	96.71	101.09	9776.4	8017.9	25.573	2994	42709	82	4.4
70	96.53	123.04	11877.1	9544.6	28.843	3160	44773	80.4	3.8
75	96.12	147.24	14152.7	11353.3	32.616	3324	55471	80.2	3.9
80	95.8	173.48	16619.4	13192.8	36.181	3482	61936	79.4	3.7
85	95.34	202.6	19315.9	15123.2	39.762	3632	67124	78.3	3.5
90	94.98	232	22035.4	16985.1	43.160	3758	72221	77.1	3.3
95	94.48	263.57	24902.1	18933.3	46.514	3887	75435	76	3.0
100	92.75	305.31	28410.3	21160.9	50.670	3988	82602	74.5	2.9

I = Current, P = Input Power, = Electrical Efficiency, T = Thrust, N = Rotational Speed. Data measured with input voltage of 96 V at 25C and sea level; rotational speed adjusted by throttle.

The above data are theoretical values when the input voltage is 96 V (for reference only). In the case of room temperature of 25C and no additional cooling device: current over 305 A is a non-working zone; 101-305 A is a short-term (about 10-30 s) working zone; below 101 A is a sustainable working zone. Control motor running time based on working environment temperature and heat dissipation conditions.

Drawing and Mount Holes

Overall diameter shown: 120.5
Length shown: 101; additional segment shown: 4
Diameters shown: 70 and 45
Propeller pattern: 34 – M5*6; center bore: 11
Mounting patterns shown: 60 and 40; note: 16 – M5 20 mm
Additional drawing notes: cable exit location marked; 34; 6 – 5.1 (+0.05/0); 50; 34; 6; 11 (+0.03/-0.01); 6 – 10; 0.5; 30

Details

MAD V185 IPE V1.0 60KV eVTOL motor uses an M5 x6 mounting pattern and a 101 mm overall length for fit and installation planning.

MAD V185 IPE V1.0 60KV motor documentation includes performance curves and a 24S data table to help match props and power setups.

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VTOL motor / KV	MAD V185 IPE 60KV
VTOL prop	Fluxer VTOL 45 x 17.5
VTOL ESC	MAD AMPX 300A (12-24S)
VTOL battery (LiPo) / voltage	24S (4.3 V/S) / 84-104 V
VTOL thrust per motor	25 kg to 35 kg
Recommended takeoff weight (4 rotors)	120 kg

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MAD V185 IPE V1.0 60KV eVTOL Airplane Drone Motor, IP35, 21 Pole Pairs, 120.5 x 105 mm