Overview

MAD X5225 (Long Shaft) IPE is an eVTOL airplane drone motor designed for efficiency-focused endurance flying and operation in harsh conditions. The available performance sheet is for a 225KV configuration on 12S LiPo (nominal), with propeller-dependent thrust and temperature limits.

Key Features

225KV configuration (as labeled on the performance sheet).
Anticorrosive stator.
Varnished wire degree: 220C.
Degree of protection: IP35.
Centrifugal heat dissipation: YES.
Precision balance specs listed for rotor and motor (mg-level).

Specifications

Motor Data

Motor model	MAD X5225 IPE V1.0
KV	225 KV
Number of pole pairs	14
Stator	Anticorrosive
Varnished wire degree	220C
Motor balance (temperature)	180C
Motor size	D:60 x 111 mm
Degree of protection	IP35
Cable length	100 mm, 14# AWG (black) silicone
Centrifugal heat dissipation	YES
Rotor balance	<= 5 mg
Motor balance (residual unbalance)	<= 10 mg
Propeller mounting	M8 nut
Shaft diameter	IN: 10 mm
Motor mounting holes	D:30 M4 x 4, D:44 M4 x 4
Bearing	EZ0 6900ZZ x1; EZO 6800ZZ x2
Disruptive test	500 V

Drawing and Mount Holes (as marked)

Outer diameter	60
Overall length	111
Body length segments	56, 55
Front feature diameter	14
Shaft step diameter	8
Shaft lengths (marked)	39.2, 27.5
Thread	M8 x 1
Front face holes	8-M4
Front face diameters (marked)	44, 30
Plate features (marked)	4-4.2, 74, 70, 44, 3.5, 8.1, 85, 19

Performance Sheet (12S)

Nominal voltage	12S LiPo battery
No load current	2.45A / 20V
Internal resistance	25 m
Motor weight	506 g
Maximum current	68.3 A
Maximum power	2877 W
Maximum torque	2.73 Nm
Maximum thrust	10.2 kg
Recommended ESC	MAD AMPX 80A (5-14S)
Recommended propellers	19×10, 20×10
Single rotor take-off weight	3 kg ~ 4.5 kg
UAV take-off weight (12S-36V)	18 kg (quadcopter); 27 kg (hexacopter); 36 kg (octocopter)
Max (temperature limit label)	105C

Test Data Table (12S, FALCON 19×10)

Throttle (%)	Voltage (V)	Current (A)	Input Power (W)	Output Power (W)	Torque (Nm)	RPM	Thrust (gf)	Efficiency (gf/W)
30	44.28	4.12	182.4	77.7	0.270	2749	1113	6.1
35	44.18	5.75	254.0	130.0	0.380	3268	1573	6.2
40	44.13	7.71	340.2	191.7	0.493	3714	2061	6.1
45	44.04	9.69	426.7	257.6	0.596	4128	2477	5.8
50	43.96	11.98	526.6	336.7	0.716	4490	2910	5.5
55	43.89	14.5	636.4	420.8	0.824	4877	3336	5.2
60	43.8	17.83	781.0	541.1	0.987	5235	4000	5.1
65	43.62	21.41	933.9	666.8	1.142	5576	4631	5.0
70	43.49	24.93	1084.2	792.1	1.276	5928	5143	4.7
75	43.32	29.57	1281.0	952.7	1.440	6318	5836	4.6
80	43.18	34.76	1500.9	1130.5	1.613	6693	6440	4.3
85	43	40.84	1756.1	1336.6	1.814	7036	7207	4.1
90	42.75	47.73	2040.5	1566.7	2.033	7359	7979	3.9
95	42.53	54.41	2314.1	1776.6	2.209	7680	8546	3.7
100	42.31	61.8	2614.8	1999.5	2.403	7946	8996	3.4

Max (label in table): 72C

Test Data Table (12S, FALCON 20×10)

Throttle (%)	Voltage (V)	Current (A)	Input Power (W)	Output Power (W)	Torque (Nm)	RPM	Thrust (gf)	Efficiency (gf/W)
30	44.3	4.2	186.1	92.9	0.322	2754	1288	6.9
35	44.22	5.99	264.9	151.4	0.442	3271	1757	6.6
40	44.16	8.07	356.4	222.0	0.571	3713	2255	6.3
45	44.05	10.25	451.5	297.3	0.693	4097	2722	6
50	43.96	12.98	570.6	395.1	0.846	4460	3254	5.7
55	43.88	16	702.1	499.6	0.991	4814	3820	5.4
60	43.74	19.61	857.7	624.1	1.151	5178	4457	5.2
65	43.61	23.4	1020.5	760.4	1.315	5522	5040	4.9
70	43.44	27.72	1204.2	910.8	1.490	5837	5716	4.7
75	43.27	32.89	1423.2	1088.5	1.672	6217	6329	4.4
80	43.07	39.2	1688.3	1305.2	1.902	6553	7273	4.3
85	42.89	45.21	1939.1	1499.9	2.077	6896	7933	4.1
90	42.66	52.36	2233.7	1724.3	2.285	7206	8758	3.9
95	42.41	60.26	2555.6	1966.6	2.504	7500	9465	3.7
100	42.13	68.29	2877.1	2213.9	2.730	7744	10211	3.5

Max (label in table): 97C

Test Notes (as stated on the sheet)

Analytical graph legend: I = Current, P = Input Power, b7 = Electrical Efficiency, T = Thrust, N = Rotational Speed.
Data measured with an input voltage of 48 V, at a temperature of 25C and sea level; rotational speed adjusted by the throttle.
Values are theoretical and for reference only.
With room temperature 25C and no additional cooling device: current over 68A is a non-working zone; 23-68A is a short-term (about 10-30s) working zone; below 23A is a sustainable working zone.
Control motor running time according to working environment temperature and heat dissipation conditions.

For wiring, ESC matching, and integration questions, contact support at [email protected] or https://rcdrone.top/.

Whats Included

Motor x1
Propeller adapter x1
M8 nut x1
Prop plate x1
Cross plate x1
4.0 mm bullet connector x3
Heat shrinkable tube x3
M4 x 12 motor screws x3
M4 x 12 mm flat head machine screw x4
M4 set screws x4
Sticker x2

Applications

eVTOL fixed-wing aircraft and endurance-focused UAV builds
12S multicopters (quadcopter/hexacopter/octocopter), based on the provided take-off weight guidance

Details

MAD X5225 long-shaft motor drawings provide key dimensions for mounting, including 111 mm overall length, an M8x1 shaft, and 4x M4 bolt holes.

The MAD X5225 motor package includes the propeller adapter, mounting plates, screws, heat-shrink, and 4.0mm bullet connectors for installation.

MAD X5225 225KV long-shaft motor includes a performance curve and key specs like 506 g weight, 10.2 kgf thrust, and 12S support for eVTOL builds.

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MAD X5225 Long Shaft IPE 225KV eVTOL Airplane Drone Motor IP35, 12S LiPo, 60x111mm, 10.2kgf, 2877W