Name: MAD 3506 IPE V1.0 Drone Motor 400KV/460KV/650KV, 87.3g, IP35, 1114in Props, 46S/6S
SKU: A2380047958
Availability: InStock

Description
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Overview

MAD 3506 IPE V1.0 drone motor (400KV / 460KV / 650KV options) is designed for single-rotor payloads of 320720 g and optimized for 1114 in carbon fiber propellers. It delivers up to 1.6 kgf maximum thrust (model dependent) with an optimized motor weight of 87.3 g.

Key Features

High thrust-to-weight design; optimized motor weight: 87.3 g
Optimized propeller range: 1114 in carbon fiber propellers
Maximum thrust (per motor, model dependent): 1.21.6 kgf
Degree of protection: IP35
Centrifugal heat dissipation: Yes
Balance specs: rotor balance 5 mg; motor balance 10 mg

Specifications

Motor Data (MAD 3506 IPE V1.0)

Motor Model	MAD 3506 IPE V1.0	Number of pole pairs	7
Stator	High-quality silicon steel sheets / high-temperature coating resistant to 180C	Varnished wire degree	150C
Motor Size	D: 42.5 28.5 mm	Magnet degree	150C
Degree of Protection	IP35	Cable Length	150 mm, 18# AWG (black) silicone
Centrifugal Heat Dissipation	Yes	Rotor Balance	5 mg
Propeller Mounting Holes	D: 12 M32, D: 15 M32	Motor Balance	10 mg
Shaft Diameter	IN: 4 mm	Motor Mounting Holes	D: 19 M32; D: 25 M32
Bearing	694ZZ*2	Disruptive test	500 V

400KV (MAD 3506 IPE 400KV)

Recommended hover thrust: 0.40.55 kgf
Maximum thrust: 1.6 kgf
Efficiency: >80%
Test setup: FLUXER PRO 13×4.4 MATT; AMPX 40A PRO (2~6S)

RPM/V	400KV	Nominal Voltage	6S lipo battery
No Load Current	0.3 A / 20 V	Internal resistance	189 m
Motor Weight	87.3 g	Product Boxed Weight	338 g (110 110 55 mm), 2 pcs/box
Maximum Current	14 A	Maximum Power	330 W
Maximum thrust	1.6 kg	Maximum Torque	0.283 Nm
Recommended ESC	MAD AMPX PRO 40A (2~6S)	Recommended Propellers	13×4.4, 14×4.8
UAV take-off weight	6S-13 in / 2 kg (quadcopter); 3 kg (hexacopter); 4 kg (octocopter)	Single rotor take-off weight	0.4 kg 0.55 kg

400KV Performance (FLUXER PRO 13×4.4 MATT, 6S, Max 71C)

Throttle (%)	Voltage (V)	Current (A)	Input Power (W)	Output Power (W)	Torque (Nxm)	RPM	Thrust (gf)	Efficiency (%)	Efficiency (gf/W)
30	23.81	0.42	9.6	7.3	0.028	2490	155	79.10	16.7
35	23.8	0.6	13.9	10.7	0.037	2809	205	82.20	15.6
40	23.79	0.97	22.7	17.6	0.051	3327	297	80.70	13.6
45	23.79	1.28	29.8	23.5	0.062	3655	366	81.80	12.7
50	23.79	1.62	38.1	29.8	0.072	3948	433	81.00	11.7
55	23.78	2.05	48.1	38.2	0.085	4297	513	82.60	11.1
60	23.77	2.57	60.5	48.0	0.098	4665	602	82.10	10.3
65	23.75	3.16	74.9	59.2	0.113	5003	699	82.40	9.7
70	23.74	3.88	91.7	73.1	0.130	5372	811	82.40	9.1
75	23.72	4.63	109.3	86.5	0.145	5692	908	81.50	8.6
80	23.7	5.54	130.9	102.7	0.163	6008	1026	80.90	8.1
85	23.69	6.35	149.7	116.6	0.177	6302	1110	80.20	7.6
90	23.67	7.41	174.7	134.4	0.195	6586	1226	79.20	7.2
95	23.66	8.59	202.7	152.6	0.212	6877	1339	77.40	6.8
100	23.62	10.26	241.8	177.1	0.234	7231	1494	75.20	6.3

400KV Performance (FLUXER PRO 14×4.8 MATT, 6S, Max 86C)

Throttle (%)	Voltage (V)	Current (A)	Input Power (W)	Output Power (W)	Torque (Nxm)	RPM	Thrust (gf)	Efficiency (%)	Efficiency (gf/W)
30	23.8	0.51	11.8	10.2	0.041	2375	185	91.90	16.6
35	23.8	0.8	18.8	15.1	0.053	2737	256	84.30	14.3
40	23.79	1.24	28.9	23.8	0.072	3173	363	85.30	13.0
45	23.79	1.62	38.1	30.9	0.086	3444	438	84.00	11.9
50	23.77	2.13	50.2	40.1	0.101	3791	531	83.10	11.0
55	23.76	2.66	62.8	50.3	0.116	4127	620	82.80	10.2
60	23.75	3.3	77.9	62.2	0.134	4445	723	82.40	9.6
65	23.74	4.03	95.2	74.8	0.151	4748	827	81.20	9.0
70	23.7	4.94	116.5	91.1	0.173	5035	947	80.60	8.4
75	23.69	6.11	144.4	109.7	0.196	5349	1086	78.40	7.8
80	23.68	7.21	170.2	125.8	0.213	5630	1193	76.10	7.2
85	23.65	8.59	202.6	142.6	0.231	5899	1298	72.40	6.6
90	23.63	9.98	235.4	159.5	0.250	6101	1419	69.60	6.2
95	23.59	12.07	284.1	173.7	0.264	6276	1496	62.70	5.4
100	23.56	14.02	329.8	191.0	0.283	6454	1596	59.30	5.0

400KV note: The above data are theoretical values when the input voltage is 24 V, for reference only. In the case of room temperature of 25C and no additional cooling device, current over 14 A is a non-working zone; 14 A is a short-term (about 1030 s) working zone; and below 4 A is a sustainable working zone. Control motor running time according to working environment temperature and heat dissipation conditions.

460KV (MAD 3506 IPE 460KV)

Recommended hover thrust: 0.30.5 kgf
Maximum thrust: 1.2 kgf
Efficiency: >83%
Test setup: FLUXER PRO 14×4.8 MATT; AMPX 40A PRO (2~6S)

RPM/V	460KV	Nominal Voltage	46S lipo battery
No Load Current	0.36 A / 20 V	Internal resistance	200 m
Motor Weight	87.3 g	Product Boxed Weight	338 g (110 110 55 mm), 2 pcs/box
Maximum Current	9.56 A	Maximum Power	204 W
Maximum thrust	1.2 kg	Maximum Torque	0.20 Nm
Recommended ESC	MAD AMPX PRO 40A (2~6S)	Recommended Propellers	11×3.7, 13×4.4, 14×4.8
UAV take-off weight	4S-14 in / 2 kg (quadcopter); 3 kg (hexacopter); 4 kg (octocopter)	Single rotor take-off weight	0.3 kg 0.5 kg

460KV Performance (FLUXER PRO 11×3.7 MATT, 6S, Max 56C)

Throttle (%)	Voltage (V)	Current (A)	Input Power (W)	Output Power (W)	Torque (Nxm)	RPM	Thrust (gf)	Efficiency (%)	Efficiency (gf/W)
30	23.95	0.34	7.4	5.2	0.017	2960	112	71.70	15.2
35	23.95	0.53	12.0	9.3	0.025	3521	165	78.80	14.0
40	23.95	0.74	17.1	13.5	0.033	3987	216	83.50	13.2
45	23.94	0.96	22.4	17.6	0.039	4318	258	82.50	12.1
50	23.95	1.27	29.7	23.8	0.048	4773	322	83.70	11.3
55	23.93	1.71	40.4	32.5	0.059	5314	408	83.90	10.5
60	23.92	2.14	51.0	40.6	0.067	5764	481	82.90	9.8
65	23.91	2.68	63.7	51.4	0.079	6208	566	83.90	9.2
70	23.9	3.27	77.8	63.5	0.092	6622	652	84.90	8.7
75	23.89	3.98	94.7	76.2	0.103	7046	745	83.70	8.2
80	23.88	4.68	111.0	89.8	0.116	7420	834	83.90	7.8
85	23.86	5.53	131.3	106.0	0.129	7817	935	83.60	7.4
90	23.84	6.29	149.6	119.5	0.141	8190	1013	83.00	7.0
95	23.83	7.22	171.6	135.5	0.151	8572	1110	81.80	6.7
100	23.8	8.57	203.5	159.4	0.168	9048	1240	81.10	6.3

460KV Performance (FLUXER PRO 13×4.4 MATT, 4S, Max 66C)

Throttle (%)	Voltage (V)	Current (A)	Input Power (W)	Output Power (W)	Torque (Nxm)	RPM	Thrust (gf)	Efficiency (%)	Efficiency (gf/W)
30	15.94	0.29	4.0	3.3	0.016	1952	79	83.10	19.6
35	15.94	0.45	7.0	5.5	0.023	2288	116	91.80	19.4
40	15.94	0.64	9.8	8.1	0.030	2597	160	91.00	17.7
45	15.93	0.84	13.0	10.9	0.037	2853	197	90.80	16.4
50	15.93	1.18	18.2	15.5	0.046	3208	257	90.70	15.0
55	15.92	1.55	24.1	20.2	0.056	3516	317	89.30	14.0
60	15.92	1.94	30.3	25.5	0.064	3817	374	89.60	13.1
65	15.91	2.41	38.0	31.7	0.074	4070	434	88.70	12.2
70	15.9	2.82	44.2	37.4	0.084	4287	494	89.90	11.8
75	15.89	3.36	53.0	44.7	0.094	4543	561	89.40	11.2
80	15.88	4.03	63.4	52.7	0.104	4830	632	87.80	10.5
85	15.87	4.7	74.0	61.3	0.115	5092	698	87.50	9.4
90	15.85	5.38	85.2	70.1	0.125	5353	762	87.30	9.5
95	15.84	6.21	98.0	80.4	0.135	5577	847	86.50	9.1
100	15.81	7.37	116.1	94.4	0.153	5907	937	85.70	8.5

460KV Performance (FLUXER PRO 14×4.8 MATT, 4S, Max 71C)

Throttle (%)	Voltage (V)	Current (A)	Input Power (W)	Output Power (W)	Torque (Nxm)	RPM	Thrust (gf)	Efficiency (%)	Efficiency (gf/W)
30	15.95	0.37	5.8	4.5	0.023	1898	112	91.40	22.4
35	15.94	0.57	8.8	7.1	0.031	2201	158	89.10	19.8
40	15.93	0.87	13.4	11.0	0.042	2526	214	86.30	16.9
45	15.93	1.13	17.5	14.1	0.049	2756	263	86.10	16.0
50	15.94	1.52	23.9	19.3	0.061	3052	326	88.00	14.8
55	15.91	2.04	31.9	26.1	0.074	3369	406	87.20	13.5
60	15.9	2.57	40.4	33.2	0.087	3645	482	87.30	12.7
65	15.88	3.11	48.8	39.9	0.098	3892	546	85.80	11.9
70	15.88	3.72	58.7	47.2	0.110	4108	616	85.50	11.2
75	15.86	4.36	68.8	55.1	0.122	4312	684	84.80	10.5
80	15.86	5.23	82.4	65.6	0.138	4562	774	84.20	9.9
85	15.84	6.15	97.0	76.3	0.152	4797	860	83.10	9.4
90	15.82	7.07	111.3	87.0	0.166	5003	943	82.40	8.9
95	15.81	8.06	126.9	98.4	0.180	5221	1020	81.90	8.5
100	15.78	9.56	150.4	114.4	0.199	5484	1128	80.00	7.9

460KV note: The above data are theoretical values when the input voltage is 16 V, for reference only. In the case of room temperature of 25C and no additional cooling device, current over 10 A is a non-working zone; 310 A is a short-term (about 1030 s) working zone; and below 3 A is a sustainable working zone. Control motor running time according to working environment temperature and heat dissipation conditions.

650KV (MAD 3506 IPE 650KV)

Recommended hover thrust: 0.40.55 kgf
Maximum thrust: 1.5 kgf
Efficiency: >83%
Test setup: FLUXER PRO 13×4.4 MATT; AMPX 40A PRO (2~6S)

RPM/V	650KV	Nominal Voltage	4S lipo battery
No Load Current	0.5 A / 16 V	Internal resistance	112 m
Motor Weight	87.3 g	Product Boxed Weight	338 g (110 110 55 mm), 2 pcs/box
Maximum Current	17.4 A	Maximum Power	270 W
Maximum thrust	1.5 kg	Maximum Torque	0.24 Nm
Recommended ESC	MAD AMPX PRO 40A (2~6S)	Recommended Propellers	13×4.4, 14×4.8
UAV take-off weight	4S-13 in / 2 kg (quadcopter); 3 kg (hexacopter); 4 kg (octocopter)	Single rotor take-off weight	0.5 kg 0.7 kg

650KV Performance (FLUXER PRO 13×4.4 MATT, 4S, Max 71C)

Throttle (%)	Voltage (V)	Current (A)	Input Power (W)	Output Power (W)	Torque (Nxm)	RPM	Thrust (gf)	Efficiency (%)	Efficiency (gf/W)
30	15.82	0.73	11.1	9.3	0.034	2612	169	92.70	16.7
35	15.81	1.07	16.7	13.5	0.044	2972	227	86.10	14.4
40	15.8	1.68	26.1	21.3	0.058	3517	322	86.30	13.0
45	15.78	2.28	35.5	29.1	0.072	3875	409	86.70	12.2
50	15.77	2.94	45.8	37.3	0.085	4205	478	85.70	11.0
55	15.76	3.62	56.7	46.0	0.097	4510	562	85.40	10.4
60	15.75	4.39	68.5	54.1	0.108	4802	636	82.70	9.7
65	15.72	5.75	89.9	70.8	0.129	5236	784	82.60	9.1
70	15.7	6.75	105.4	82.8	0.142	5569	866	82.10	8.6
75	15.68	8.1	126.6	97.8	0.158	5904	976	80.80	8.1
80	15.65	9.55	148.9	112.9	0.174	6186	1081	79.10	7.6
85	15.62	11.08	172.6	129.1	0.191	6447	1175	77.90	7.1
90	15.59	12.91	200.8	145.8	0.207	6742	1287	75.40	6.7
95	15.56	14.48	224.9	160.9	0.220	6984	1385	74.20	6.4
100	15.5	17.44	269.9	185.9	0.243	7313	1531	71.10	5.9

650KV Performance (FLUXER PRO 14×4.8 MATT, 4S, Max 89C)

Throttle (%)	Voltage (V)	Current (A)	Input Power (W)	Output Power (W)	Torque (Nxm)	RPM	Thrust (gf)	Efficiency (%)	Efficiency (gf/W)
30	14.54	0.32	4.0	3.7	0.021	1757	95	94.50	23.6
35	14.54	0.47	6.0	5.6	0.027	2011	128	93.80	21.4
40	14.53	0.74	10.0	9.0	0.037	2349	184	91.70	18.6
45	14.53	1	14.0	11.9	0.044	2579	226	86.90	16.4
50	14.52	1.28	18.1	15.1	0.052	2796	275	88.50	16.1
55	14.52	1.72	24.4	20.4	0.063	3087	338	86.60	14.3
60	14.51	2.19	31.2	26.2	0.075	3361	402	87.50	13.4
65	14.53	2.77	39.8	32.6	0.087	3600	471	85.50	12.3
70	14.49	3.28	47.0	39.2	0.098	3827	537	86.20	11.8
75	14.48	3.88	55.8	45.4	0.108	4036	599	84.30	11.1
80	14.47	4.55	65.2	53.2	0.120	4244	664	84.30	10.5
85	14.45	5.32	76.5	62.3	0.133	4460	741	84.20	10.0
90	14.44	6.13	88.0	70.5	0.144	4665	811	82.70	9.5
95	14.42	7.07	101.4	80.1	0.157	4855	890	81.40	9.1
100	14.4	8.31	119.1	93.2	0.174	5115	993	80.30	8.6

650KV note: The above data are theoretical values when the input voltage is 16 V, for reference only. In the case of room temperature of 25C and no additional cooling device, current over 8 A is a non-working zone; 38 A is a short-term (about 1030 s) working zone; and below 3 A is a sustainable working zone. Control motor running time according to working environment temperature and heat dissipation conditions.

Whats Included

Motor 2
Propeller plate 2
3.5 mm bullet connector 6
46 adapter ring 2
Heat shrinkable tube 6
M36 motor screws 8
M310 propeller screws 4
Sticker 2

Applications

Professional aerial photography platforms
High-efficiency payload delivery
Demanding industrial UAV platforms

For custom KV options or bulk orders, contact [email protected] or visit https://rcdrone.top/.

Details

MAD 3506 IPE V1.0 motor dimensions include a 42.5 mm body diameter, 25.5 mm height, and multiple M3 mounting patterns for fit checks.

MAD 3506 IPE V1.0 motor hardware includes propeller plates, 3.5mm bullet connectors, adapter rings, heat-shrink tubing, and M3 mounting screws for installation.

MAD 3506 IPE V1.0 motor specs list a 400KV option with thrust and efficiency data across multiple 6S prop tests.

The MAD 3506 IPE V1.0 motor is listed at 460KV and 87.3g, with performance charts and test data to help with prop and setup selection.

MAD 3506 IPE V1.0 650KV drone motor specs list 4055 kgf max thrust, 1.5 kgf hover thrust, and over 83% efficiency.

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MAD 3506 IPE V1.0 Drone Motor 400KV/460KV/650KV, 87.3g, IP35, 1114in Props, 46S/6S