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

Description

Overview

MAD V68 IPE V1.0 is a 230KV eVTOL drone motor designed to carry payloads of 56.5 kg per rotor, with maximum thrust up to 13.9 kg per rotor. Unit motor weight is 378 g. It is intended for 1520 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: 5.07.0 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	150C
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 M34, 18 M34, 22 M34
Motor Mounting Holes	D:25 M34, D:30 M44
Motor Balance (listed)	150C

Additional Electrical / Performance Specs

Nominal Voltage	12S lipo battery
No Load Current	2.1 A / 20 V
Internal resistance	30.5 m
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	22×6.6, 22.1×7.4
Recommended ESC	MAD AMPX 80A (5-14S)
Single rotor take-off weight	5 kg ~ 7 kg

Drawing Dimensions (as labeled)

Labeled dimensions	72, 37.5, 2, 48, 4
Motor mounting hole patterns (labeled)	30-M44; 25-M34
Propeller mounting hole patterns (labeled)	22-M34; 18-M34; 12-M34

Analytical Graph of Motor Operation (test conditions)

• Measured with an input voltage of 48 V, at a temperature of 25C and sea level.
• The rotational speed was adjusted by the throttle.
• Legend: I = Current, P = Input Power, = Electrical Efficiency, T = Thrust, N = Rotational Speed

Operation Data (MAD V68 IPE 230KV + FLUXER PRO 22×6.6 MATT + AMPX 80A (5-14S), 12S)

Throttle (%)	Voltage (V)	Current (A)	Input Power (W)	Output Power (W)	Torque (Nm)	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 22.1×7.4 VTOL + AMPX 80A (5-14S), 12S)

Throttle (%)	Voltage (V)	Current (A)	Input Power (W)	Output Power (W)	Torque (Nm)	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 25C and without additional cooling, current over 85 A is a non-working zone; 3185 A is a short-term (about 1030 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 [email protected] or visit https://rcdrone.top/.

Whats Included

• Motor x1
• Propeller Plate x1
• Prop Adapter x1
• 46 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 22×6.6 / 22.1×7.4	MAD AMPX 80A (5-14S)

VTOL Battery (Lipo) / Voltage	VTOL Thrust Per Motor (kg)	Recommended takeoff weight (4 rotors)
12S (4.3 V/S) / 4252 V	5 kg ~ 7 kg	23 kg

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

Details

The MAD V68 IPE V1.0 motor uses multiple M3 and M4 mounting hole patterns to help match common eVTOL frames and hubs.

The MAD V68 IPE V1.0 motor comes with a propeller plate, prop adapter, adapter ring, bullet connectors, heat shrink tubing, mounting screws, and stickers for a complete install.

The MAD V68 IPE V1.0 motor is rated 230KV for 5070V setups, with a listed weight of 378g and up to 13.9kgf thrust.