MAD V128 IPE V2.0 eVTOL UAV Drone Motor 50KV/65KV 24S, 1910g, 6062kgf Max Thrust

Description

Overview

MAD V128 is an eVTOL UAV drone motor designed for heavy-payload, long-endurance aircraft applications. It supports up to 62 kgf maximum thrust per rotor (recommended hover thrust 2027 kgf), with an optimized motor weight of 1910 g.

Key Features

• Heavy lift capability: up to 62 kgf maximum thrust; recommended hover thrust 2027 kgf
• Lightweight design: 1910 g motor weight
• Centrifugal heat dissipation: YES
• Optional ENCR (Electronic Control)

Specifications

Motor Data (MAD V128 IPE V2.0)

Motor model	MAD V128 IPE V2.0
Number of pole pairs	19
Stator	Anticorrosive
Varnished wire degree	220C
Magnet degree	180C
Motor size	D:145 x 59 mm
Degree of protection	IP35
Cable length	150 mm (extended enameled wires)
Centrifugal heat dissipation	YES
Rotor balance	<=10 mg
Motor balance	<=20 mg
Propeller mounting holes	D:24 M4 x 4; D:30 M5 x 4
Motor mounting holes	D:50 M6 x 4
Shaft diameter	IN: 20 mm
Bearing	6904ZZ*2
Disruptive test	500 V

Mounting / Drawing Dimensions (selected)

Outer diameter (drawing)	D144.6
Motor mounting pattern (drawing)	50-M6*4
Prop mounting pattern (drawing)	30-M4*4
Hub detail (drawing)	30-M5*4; 24-M4*4; 7.2; 4.2
Additional detail (drawing)	24; 30; 4.1; 5.2; 10; 44; thickness 3
Body width (drawing)	50
Side feature (drawing)	43

65KV (24S) Performance Summary

RPM/V	65 KV
No-load current	3.5A/30V
Motor weight	1910 g
Nominal voltage	24S lipo battery
Internal resistance	18.4 mOhm
Maximum current	238.1 A
Maximum power	19854 W
Maximum torque	30.2 Nm
Maximum thrust	62 kg
Recommended ESC	MAD AMPX 300A (12-24S)
Recommended propellers	42×14
Single rotor take-off weight	20kg ~ 27kg
Product boxed weight	2860g (260 x 210 x 120 mm)
Efficiency (sheet)	>82%
24S temperature limit shown	MAX 139C

50KV (24S) Performance Summary

RPM/V	50 KV
No-load current	2.45A/30V
Motor weight	1910 g
Nominal voltage	24S lipo battery
Internal resistance	34 mOhm
Maximum current	165 A
Maximum power	15886 W
Maximum torque	25.4 Nm
Maximum thrust	60 kg
Recommended ESC	MAD AMPX 200A (12-24S)
Recommended propellers	40×13.1
Single rotor take-off weight	20kg ~ 27kg
Product boxed weight	2860g (260 x 210 x 120 mm)
Efficiency (sheet)	>85%
24S temperature limits shown	MAX 116C; MAX 98C

For ESC/prop matching and wiring/connector questions, contact [email protected] or visit https://rcdrone.top/.

Recommended Setup (Solution)

VTOL Motor/KV	MAD V128 IPE 50KV
VTOL Prop	Fluxer VTOL 40×13.1
VTOL ESC	MAD AMPX 200A (12-24S)
VTOL Battery (LiPo) / Voltage	24S (4.3V/S) / 84104V
VTOL thrust per motor	20kg ~ 27kg
Recommended takeoff weight (4 axes)	80kg

Alternative VTOL prop listed: Fluxer VTOL 42×14. Note: For a coaxial configuration, a total thrust loss of 25% should be considered.

Whats Included

• Motor x1
• Propeller Plate x1
• Prop Adapter x1
• 8.0mm Bullet Connector x3
• Heat Shrinkable Tube x3
• M6*25 Motor Screws x4
• M4*12 Prop Adapter Screws x4
• M4*20 Propeller Screws x4

Applications

• Surveying
• Logistics
• Agriculture
• Other heavy-payload, long-endurance UAV aircraft applications

Performance Data (from provided motor sheets)

Test / graph notes

• Analytical Graph of Motor Operation variables: I (current), P (input power), (electrical efficiency), T (thrust), N (rotational speed).
• Data notes (as stated): measured with input voltage 96 V, at 25C and sea level; rotational speed adjusted by throttle.
• Maximum thrust may depend on battery level, propeller type, air pressure and other conditions.

65KV (MAD V128 IPE 65KV, 24S, sheet header: CB2 42×14 MATT, AMPX 300A (12-24S))

Throttle [%]	Voltage [V]	Current [A]	Input Power [W]	Output Power [W]	Torque [N*m]	RPM	Thrust [gf]	Efficiency [%]	Efficiency [gf/W]
30	88.51	9.61	850.7	600.8	3.403	1686	7638	70.63	9.0
35	88.54	12.88	1140.7	856.2	4.297	1903	9670	75.03	8.5
40	88.53	17.39	1539.7	1174.9	5.278	2126	12140	76.29	7.9
45	88.53	25.14	2226.0	1761.7	7.024	2395	15386	79.11	6.9
50	88.48	36.91	3266.1	2498.2	8.915	2676	19360	76.52	5.9
55	88.32	44.43	3924.0	3333.4	10.880	2926	23402	84.99	6.0
60	88.36	55.25	4881.9	4270.2	12.885	3165	27519	87.59	5.6
65	88.33	74.41	6573.0	5302.4	14.972	3382	31769	80.69	4.8
70	88.17	86.92	7663.7	6324.7	16.779	3600	36173	82.56	4.7
75	88.18	104.89	9248.9	7803.7	19.543	3813	41327	84.37	4.5
80	88.09	133.99	11803.7	9308.3	22.097	4023	46276	78.86	3.9
85	87.91	150.12	13196.4	11040.1	25.122	4197	50971	83.67	3.9
90	87.8	176.23	15473.6	12899.3	28.136	4378	55732	83.36	3.6
95	87.72	211.96	18593.6	13956.4	29.434	4528	60244	75.06	3.2
100	83.38	238.12	19854.5	14438.5	30.190	4567	62039	72.72	3.1

65KV note (as stated): values are theoretical at 96 V for reference only. With no additional cooling at 25C, current over 238 A is non-working zone; 74238 A is short-term (about 1030 s) working zone; below 74 A is sustainable working zone. Control running time according to environment temperature and heat dissipation conditions.

50KV (MAD V128 IPE 50KV, 24S, sheet header: FLUXER PRO 40×13.1 GLOSSY, AMPX 200A (12-24S))

Dataset A (sheet shows: 24S MAX 98C)

Throttle [%]	Voltage [V]	Current [A]	Input Power [W]	Output Power [W]	Torque [N*m]	RPM	Thrust [gf]	Efficiency [%]	Efficiency [gf/W]
30	88.77	5.43	482.0	360.6	2.508	1373	4605	74.8	9.6
35	88.73	7.67	680.6	501.8	3.025	1584	6200	73.7	9.1
40	88.73	10.12	897.9	717.8	3.886	1764	7604	79.9	8.5
45	88.69	13.31	1180.5	962.8	4.710	1952	9339	81.6	7.9
50	88.65	18.04	1599.2	1316.0	5.829	2156	11735	82.3	7.3
55	88.58	23.51	2082.5	1803.8	7.216	2387	14521	86.6	7.0
60	88.48	30.54	2702.2	2367.0	8.680	2604	17625	87.6	6.5
65	88.42	37.98	3358.2	2950.0	10.050	2803	20350	87.8	6.1
70	88.34	46.58	4114.9	3659.9	11.642	3002	23401	88.9	5.7
75	88.21	56.52	4985.6	4297.6	12.842	3196	26851	86.2	5.4
80	88.11	67.6	5956.2	5021.1	14.157	3387	30300	84.3	5.1
85	87.98	80.41	7074.5	5822.3	15.527	3581	33893	82.3	4.8
90	87.83	96.39	8465.9	6891.2	17.443	3773	38225	81.4	4.5
95	88.13	113.42	9995.7	8006.6	19.135	3996	42544	80.1	4.3
100	87.46	131.22	11476.5	8986.1	20.599	4166	48549	78.3	4.2

Dataset B (sheet shows: 24S MAX 116C)

Throttle [%]	Voltage [V]	Current [A]	Input Power [W]	Output Power [W]	Torque [N*m]	RPM	Thrust [gf]	Efficiency [%]	Efficiency [gf/W]
30	97.77	6.41	626.7	476.3	3.012	1510	5720	76	9.1
35	97.76	8.77	857.4	681.6	3.787	1719	7394	79.5	8.6
40	97.71	11.79	1152.0	946.9	4.725	1914	9263	82.2	8.0
45	97.7	15.79	1542.7	1311.3	5.896	2124	11506	85	7.5
50	97.66	21.22	2072.3	1742.8	7.011	2374	13989	84.1	6.8
55	97.6	28.42	2773.8	2427.1	8.847	2620	17665	87.5	6.4
60	97.47	36.62	3569.4	3198.2	10.736	2845	21049	89.6	5.9
65	97.38	45.39	4420.1	3907.4	12.187	3062	24705	88.4	5.6
70	97.28	54.93	5343.6	4681.0	13.633	3279	28433	87.4	5.3
75	97.15	66.3	6441.0	5429.8	14.901	3480	31669	84.3	4.9
80	97.03	80.19	7780.8	6426.9	16.642	3688	36031	82.6	4.6
85	96.85	96.35	9331.5	7427.9	18.217	3894	40981	79.6	4.4
90	96.62	114.79	11091.0	8628.8	20.094	4101	45965	77.8	4.1
95	96.43	136.12	13126.1	9989.0	22.299	4278	51733	76.1	3.9
100	96.08	165.34	15885.9	11962.1	25.347	4507	59518	75.3	3.7

50KV note (as stated): values are theoretical at 96 V for reference only. With no additional cooling at 25C, current over 165 A is non-working zone; 45165 A is short-term (about 1030 s) working zone; below 45 A is sustainable working zone. Control running time according to environment temperature and heat dissipation conditions.

Details

The MAD V128 IPE V2.0 eVTOL UAV motor uses a 50 mm mounting pattern with M6 holes and a 30 mm pattern with M4 holes for straightforward integration.

The MAD V128 IPE V2.0 motor package includes a propeller plate, prop adapter, 8mm bullet connectors, heat-shrink tubing, and mounting hardware for installation.

The MAD V128 IPE V2.0 drone motor spec sheet lists key figures like 65KV rating, thrust range, and efficiency alongside performance curves.

MAD V128 IPE V2.0 eVTOL UAV motor documentation lists a 50KV rating, 2027V operating range, and performance curves for setup planning.