FM4310 Outrunner Brushless DC Motor for Multirotor Drones and Quadrotor

product details

Parameter:

Motor model：FM4310

Structure form：18N24P

Weight：155g

Stator core size：φ43*10 mm

Dimensions：φ50.4*29.5 mm

Outgoing line：18AWG*L500 mm

Spindle diameter：IN: φ6 mm OUT:φ3 mm

Dynamic balance standard：≤8mg

DRAWING

1625823pm4

TEST REPORT

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Max thrust		Max power
FM4310 KV330		40A (4S-6S)	P1865 18 inch straight propeller		Multi-rotor,VTOL	1.1KG-1.4KG uniaxial	2.8KG		469W
Load test data						Lithium Battery :6S 22.2V
Voltage(V)	Thrust(g）	Current(A)		RPM	Power(W)		Efficien cy(g/W	Torque (N.m)	Accelerator
21.94	508	1.96		2386	43.00		11.81	0.17	40%
21.91	654	2.5		2643	54.78		11.94	0.20	45%
21.91	822	3.28		2896	71.86		11.44	0.24	50%
21.91	960	4.62		3182	101.22		9.48	0.30	55%
21.86	1173	5.55		3472	121.32		9.67	0.33	60%
21.85	1201	7.26		3655	158.63		7.57	0.41	65%
21.84	1499	7.72		3883	168.60		8.89	0.41	70%
21.83	1679	9.15		4103	199.74		8.41	0.46	75%
21.83	1852	10.68		4309	233.14		7.94	0.52	80%
21.81	2046	12.31		4520	268.48		7.62	0.57	85%
21.77	2269	14.08		4699	306.52		7.40	0.62	90%
21.74	2386	16.18		4878	351.75		6.78	0.69	95%
21.74	2568	17.96		5050	390.45		6.58	0.74	100%

Load test data						Lithium Battery :6S 24V
Voltage(V)	Thrust(g）	Current(A)		RPM	Power(W)		Efficien cy(g/W	Torque (N.m)	Accelerator
23.72	605	2.12		2560	50.29		12.03	0.19	40%
23.71	756	2.89		2845	68.52		11.03	0.23	45%
23.68	964	4.03		3164	95.43		10.10	0.29	50%
23.69	1130	5.04		3425	119.40		9.46	0.33	55%
23.68	1313	6.34		3688	150.13		8.75	0.39	60%
23.67	1490	7.41		3883	175.39		8.50	0.43	65%
23.63	1676	8.8		4107	207.94		8.06	0.48	70%
23.64	1846	10.34		4339	244.44		7.55	0.54	75%
23.59	2065	11.94		4553	281.66		7.33	0.59	80%
23.57	2318	13.78		4743	324.79		7.14	0.65	85%
23.57	2513	15.96		4931	376.18		6.68	0.73	90%
23.54	2631	17.93		5118	422.07		6.23	0.79	95%
23.49	2846	19.97		5280	469.10		6.07	0.85	100%

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Max thrust		Max power
FM4310 KV330		40A (4S-6S	F1855 18 inch folding propeller		Multi-rotor,VTOL	1.2KG-1.6KG uniaxial	3.3KG		600W
Load test data						Lithium Battery :6S 22.2V
Voltage(V)	Thrust(g）	Current(A)		RPM	Power(W)		Efficien cy(g/W	Torque (N.m)	Accelerator
21.93	643	2.38		2324	52.19		12.32	0.21	40%
21.89	828	3.14		2567	68.73		12.05	0.26	45%
21.89	1027	4.37		2871	95.66		10.74	0.32	50%
21.88	1230	5.56		3097	121.65		10.11	0.38	55%
21.88	1425	6.84		3329	149.66		9.52	0.43	60%
21.87	1573	8.09		3519	176.93		8.89	0.48	65%
21.82	1776	9.69		3732	211.44		8.40	0.54	70%
21.82	2001	11.59		3941	252.89		7.91	0.61	75%
21.77	2271	13.77		4114	299.77		7.58	0.70	80%
21.77	2420	16.26		4290	353.98		6.84	0.79	85%
21.72	2658	18.36		4503	398.78		6.67	0.85	90%
21.72	2826	20.19		4633	438.53		6.44	0.90	95%
21.67	3002	22.34		4780	484.11		6.20	0.97	100%

Load test data						Lithium Battery :6S 24V
Voltage(V)	Thrust(g）	Current(A)		RPM	Power(W)		Efficien cy(g/W	Torque (N.m)	Accelerator
23.71	759	2.71		2457	64.25		11.81	0.25	40%
23.71	998	3.95		2789	93.65		10.66	0.32	45%
23.69	1225	5.2		3084	123.19		9.94	0.38	50%
23.69	1400	6.43		3315	152.33		9.19	0.44	55%
23.68	1585	7.64		3526	180.92		8.76	0.49	60%
23.64	1773	9.21		3743	217.72		8.14	0.56	65%
23.62	1978	10.97		3970	259.11		7.63	0.62	70%
23.59	2209	12.93		4172	305.02		7.24	0.70	75%
23.56	2447	15.17		4350	357.41		6.85	0.78	80%
23.53	2705	17.52		4524	412.25		6.56	0.87	85%
23.52	2873	19.75		4712	464.52		6.18	0.94	90%
23.48	3129	22.58		4859	530.18		5.90	1.04	95%
23.44	3352	25.62		4985	600.53		5.58	1.15	100%

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Max thrust		Max power
FM4310 KV360		60A (4S-6S)	P1865 18 inch straight propeller		Multi-rotor,VTOL	1.2KG-1.6KG Uh1aX1al	3.5KG		664W
Load test data						Lithium Battery :6S 22.2V
Voltage(V)	Thrust(g）	Current(A)		RPM	Power(W)		Efficien cy(g/W	Torque (N.m)	Accelerator
21.93	714	2.63		2655	57.68		12.38	0.21	40%
21.89	931	3.94		3028	86.25		10.79	0.27	45%
21.88	1160	5.19		3358	113.56		10.22	0.32	50%
21.88	1365	6.53		3629	142.88		9.55	0.38	55%
21.86	1558	8.02		3895	175.32		8.89	0.43	60%
21.83	1759	9.52		4127	207.82		846	0.48	65%
21.82	1958	11.33		4373	247.22		7.92	0.54	70%
21.78	2130	13.06		4629	284.45		7.49	0.59	75%
21.78	2342	15.11		4863	329.10		7.12	0.65	80%
21.71	2583	17.67		5066	383.62		6.73	0.72	85%
21.71	2802	20.18		5264	438.11		6.40	0.79	90%
21.66	3009	22.79		5483	493.63		6.10	0.86	95%
21.67	3249	25.52		5645	553.02		5.88	0.94	100%

Load test data						Lithium Battery :6S 24V
Voltage(V)	Thrust(g）	Current(A)		RPM	Power(W)		Efficien cy(g/W	Torque (N.m)	Accelerator
23.71	833	3.08		2850	73.03		11.41	0.24	40%
23.72	1074	4.46		3251	105.79		10.15	0.31	45%
23.65	1323	5.79		3585	136.93		9.66	0.36	50%
23.68	1506	7.24		3853	171.44		8.78	0.42	55%
23.61	1758	8.9		4127	210.13		8.37	0.49	60%
23.62	1976	10.68		4377	252.26		7.83	0.55	65%
23.60	2218	12.66		4642	298.78		7.42	0.61	70%
23.56	2453	14.83		4887	349.39		7.02	0.68	75%
23.56	2672	17.13		5102	403.58		6.62	0.76	80%
23.52	2918	19.84		5331	466.64		6.25	0.84	85%
23.47	3149	22.47		5538	527.37		5.97	0.91	90%
23.46	3389	25.38		5749	595.41		5.69	0.99	95%
23.42	3596	28.37		5912	664.43		5.41	1.07	100%

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Max thrust		Max power
FM4310 KV400		60A (4S-6S)	P1651 16 inch straight propeller		Multi-rotor,VTOL	1.1KG-1.4KG uniaxial	3.1KG		525W
Load test data						Lithium Battery :6S 22.2V
Voltage(V)	Thrust(g）	Current(A)		RPM	Power(W)		Efficien cy(g/W	Torque (N.m)	Accelerator
21.93	568	2.26		2995	49.56		11.46	0.16	40%
21.93	736	3.12		3376	68.42		10.76	0.19	45%
21.89	900	4.06		3707	88.87		10.13	0.23	50%
21.89	1050	5.1		4005	111.64		9.41	0.27	55%
21.87	1245	6.21		4343	135.81		9.17	0.30	60%
21.87	1412	7.46		4616	163.15		8.65	0.34	65%
21.84	1617	9.01		4936	196.78		8.22	0.38	70%
21.81	1758	10.36		5192	225.95		7.78	0.42	75%
21.81	1961	12.2		5483	266.08		7.37	0.46	80%
21.78	2165	13.85		5736	301.65		7.18	0.50	85%
21.75	2368	15.84		5983	344.52		6.87	0.55	90%
21.75	2568	17.96		6253	390.63		6.57	0.60	95%
21.72	2796	20.01		6472	434.62		6.43	0.64	100%

Load test data						Lithium Battery :6S 24V
Voltage(V)	Thrust(g）	Current(A)		RPM	Power(W)		Efficien cy(g/W	Torque (N.m)	Accelerator
23.72	661	2.53		3253	60.01		11.01	0.18	40%
23.68	841	3.36		3624	79.56		10.57	0.21	45%
23.68	1015	4.43		3963	104.90		9.68	0.25	50%
23.68	1176	5.54		4257	131.19		8.96	0.29	55%
23.67	1476	6.86		4607	162.38		9.09	0.34	60%
23.67	1576	8.33		4911	197.17		7.99	0.38	65%
23.64	1769	9.71		5192	229.54		7.71	0.42	70%
23.63	1989	11.57		5508	273.40		7.28	0.47	75%
23.59	2198	13.38		5802	315.63		6.96	0.52	80%
23.59	2427	15.29		6078	360.69		6.73	0.57	85%
23.55	2676	17.59		6332	414.24		6.46	0.62	90%
23.52	2893	19.85		6609	466.87		6.20	0.67	95%
23.48	3103	22.36		6845	525.01		5.91	0.73	100%

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Max thrust		Max power
FM4310 KV460		60A (4S-6S)	P1447 14 inch straight propeller		Multi-roto,VTOL	1.1KG-1.3KG uniaxial	3.0KG		586W
Load test data						Lithium Battery :6S 22.2V
Voltage(V)	Thrust(g）	Current(A)		RPM	Power(W)		Efficien cy(g/W	Torque (N.m)	Accelerator
21.88	575	2.58		3738	56.45		10.19	0.14	40%
21.89	709	3.58		4162	78.37		9.05	0.18	45%
21.89	852	4.42		4532	96.75		8.81	0.20	50%
21.88	1012	5.47		4873	119.68		8.46	0.23	55%
21.87	1152	6.83		5275	149.37		7.71	0.27	60%
21.84	1341	8.26		5645	180.40		7.43	0.31	65%
21.83	1543	10.17		5998	222.01		6.95	0.35	70%
21.83	1728	11.49		6357	250.83		6.89	0.38	75%
21.76	1937	13.52		6689	294.20		6.58	0.42	80%
21.75	2138	15.68		7008	341.04		6.27	0.46	85%
21.73	2356	17.72		7295	385.06		6.12	0.50	90%
21.71	2506	19.85		7630	430.94		5.82	0.54	95%
21.67	2707	22.29		7908	483.02		5.60	0.58	100%

Load test data						Lithium Battery :6S 24V
Voltage(V)	Thrust(g）	Current(A)		RPM	Power(W)		Efficien cy(g/W	Torque (N.m)	Accelerator
23.73	666	3.13		3995	74.27		8.97	0.18	40%
23.69	819	4.04		4451	95.71		8.56	0.21	45%
23.68	1005	5.28		4859	125.03		8.04	0.25	50%
23.67	1153	6.3		5214	149.12		7.73	0.27	55%
23.66	1345	7.76		5619	183.60		7.33	0.31	60%
23.63	1535	9.19		5998	217.16		7.07	0.35	65%
23.61	1737	11.06		6373	261.13		6.65	0.39	70%
23.57	1935	12.72		6743	299.81		6.45	0.42	75%
23.57	2125	14.87		7078	350.49		6.06	0.47	80%
23.54	2382	17.34		7404	408.18		5.84	0.53	85%
23.52	2609	19.78		7737	465.23		5.61	0.57	90%
23.46	2807	22.35		8075	524.33		5.35	0.62	95%
23.45	3033	24.99		8373	586.02		5.18	0.67	100%

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Max thrust		Max power
FM4310 KV600		60A (4S-6S)	P1555 15 inch straight propeller		Multi-rotor,VTOL	1.0KG-1.3KG uniaxial	2.6KG		478W
Load test data						Lithium Battery :4S 14.8V
Voltage(V)	Thrust(g）	Current(A)		RPM	Power(W)		Efficien cy(g/W	Torque (N.m)	Accelerator
14.51	526	3.28		3061	47.59		11.05	0.15	40%
14.49	633	4.35		3406	63.03		10.04	0.18	45%
14.48	799	5.77		3806	83.55		9.56	0.21	50%
14.47	970	7.22		4127	104.47		9.28	0.24	55%
14.42	1174	8.75		4447	126.18		9.30	0.27	60%
14.42	1271	10.66		4748	153.72		8.27	0.31	65%
14.38	1445	12.51		5020	179.89		8.03	0.34	70%
14.36	1554	14.37		5292	206.35		7.53	0.37	75%
14.35	1710	16.76		5600	240.51		7.11	0.41	80%
14.31	1910	19.41		5871	277.76		6.88	0.45	85%
14.27	2075	21.91		6138	312.66		6.64	0.49	90%
14.25	2256	24.82		6397	353.69		6.38	0.53	95%
14.22	2425	27.81		6618	395.46		6.13	0.57	100%

Load test data						Lithium Battery :4S 16V
Voltage(V)	Thrust(g）	Current(A)		RPM	Power(W)		Efficien cy(g/W	Torque (N.m)	Accelerator
15.69	527	3.73		3349	58.52		9.00	0.17	40%
15.67	668	4.85		3713	76.00		8.79	0.20	45%
15.67	866	6.36		4077	99.66		8.69	0.23	50%
15.64	1010	7.58		4350	118.55		8.52	0.26	55%
15.60	1133	9.42		4694	146.95		7.71	0.30	60%
15.58	1358	11.66		5061	181.66		7.48	0.34	65%
15.58	1513	14.09		5389	219.52		6.89	0.39	70%
15.55	1690	1,645		5690	255.80		6.61	0.43	75%
15.53	1890	19.07		5969	296.16		6.38	0.47	80%
15.47	2072	21.37		6253	330.59		6.27	0.50	85%
15.45	2255	24.24		6489	374.51		6.02	0.55	90%
15.41	2420	27.46		6780	423.16		5.72	0.60	95%
15.38	2621	31.11		7028	478.47		5.48	0.65	100%