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0102030405

Flycci Motor UM1115 brushless motor multi-rotor long endurance UAV heavy load aerial mapping

product details

Parameter:

Motor model: UM1115

Structure form: 36N40P

Weight: 826g

Stator core size: φ110*15mm

Dimensions: φ120.2* 44mm

Spindle diameter: φ15mm

Output shaft diameter: φ3mm

Dynamic balance standard: ≤10mg

UM1115 KV85

Recommended for lithium battery: 12S-14S

Recommended propeller: 38-40 inches

Multi-rotor take-off weight: 8KG-12KG/ shaft

UM1115 KV95

Recommended for lithium battery: 12S-14S

Recommended propeller: 38-40 inches

Multi-rotor take-off weight: 9KG-12KG/ shaft

UM1115 KV110

Recommended for lithium battery: 12S-14S

Recommended propeller: 36-38 inches

Multi-rotor take-off weight: 8KG-12KG/ shaft

DRAWING

TEST REPORT

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Rated power	Max thrust	Max power
UM1115 KV110		120A	P3812 38 inch straight propeller		Multi-rotor drone	9.0KG-12KG/shaft	1460W	22.6KG	4.3KW
Load test data						Lithium Battery :12S
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
45.17	6292	12.03		1735	543.40		11.5791	2.9910	40%
45.11	7671	15.82		1912	713.64		10.7491	3.5645	45%
44.91	9104	20.67		2089	92829		9.8073	4.2437	50%
44.85	10731	27.11		2282	1215.88		8.8257	5.0884	55%
44.66	12247	33.52		2462	1497.00		8.1810	5.8068	60%
44.40	13891	40.77		2619	1810.19		7.6738	6.6007	65%
44.20	15399	48.9		2762	2161.38		7.1246	7.4733	70%
44.15	16809	57.76		2898	2550.10		6.5915	8.4036	75%
43.81	18599	66.17		3015	2898.91		6.4159	9.1823	80%
43.65	19733	76.35		3135	3332.68		5.9211	10.1522	85%
43.30	20686	87.4		3247	3784.42		5.4661	11.1306	90%
43.10	22045	98.59		3341	4249.23		5.1880	12.1461	95%
43.17	22601	99.1		3418	4278.15		5.2829	11.9533	100%
The above figures are from the actual melting room: sea level requires height, E8-2023 test platform

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Rated power	Max thrust	Max power
UM1115 KV110		120A	F34128 34 inch folding propeller		Multi-rotor drone	7KG-11KG/uniaxial	24.5KG		4118W
Load test data						Lithium Battery :12S 44.4V
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
44.09	4627	9.45		1774	416.65		11.11	2.24	40%
44.06	5908	13.57		2017	597.89		9.88	2.83	45%
44.01	7180	18.05		2229	794.38		9.04	3.40	50%
43.94	8835	23.63		2412	1038.30		8.51	4.11	55%
43.85	10234	29.74		2603	1304.10		7.85	4.78	60%
43.81	11487	35.12		2752	1538.61		7.47	5.34	65%
43.71	12553	42.45		2938	1855.49		6.77	6.03	70%
43.58	14337	51.33		3122	2236.96		6.41	6.84	75%
43.46	15792	60.09		3279	2611.51		6.05	7.61	80%
43.39	16892	69.94		3449	3034.70		5.57	8.40	85%
43.25	18506	80.22		3616	3469.52		5.33	9.16	90%
43.09	20408	92.29		3733	3976.78		5.13	10.17	95%
42.94	21630	105.07		3883	4511.71		4.79	11.10	100%
Load test data						Lithium Battery :12S 48V
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
47.69	5629	11.21		1928	534.60		10.53	2.65	40%
47.63	7142	16.09		2177	766.37		9.32	3.36	45%
47.56	8768	21.21		2387	1008.75		8.69	4.04	50%
47.51	10285	27.16		2592	1290.37		7.97	4.75	55%
47.42	11715	32.91		2762	1560.59		7.51	5.40	60%
47.34	13097	40.17		2955	1901.65		6.89	6.15	65%
47.25	14395	48.63		3138	2297.77		6.26	6.99	70%
47.13	16001	57.92		3323	2729.77		5.86	7.85	75%
46.99	18036	67.97		3489	3193.91		5.65	8.74	80%
46.87	19351	78.14		3687	3662.42		5.28	9.49	85%
46.74	20512	89.22		3858	4170.14		4.92	10.32	90%
46.61	22291	102.31		3971	4768.67		4.67	11.47	95%
46.43	24510	115.54		4118	5364.52		4.57	12.44	100%
The above figures are from the actual melting room: sea level requires height, E8-2023 test platform

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Rated power	Max thrust	Max power
UM1115 KV110		120A	F36120 36 inch folding propeller		Multi-rotor drone	8KG-12KG/uniaxial	26KG		5840W
Load test data						Lithium Battery :12S 44.4V
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
44.08	5168	10.31		1779	454.46		11.37	2.44	40%
44.04	6582	14.63		2024	644.31		10.22	3.04	45%
43.97	8097	20.13		2229	885.12		9.15	3.79	50%
43.88	9599	25.77		2420	1130.79		8.49	4.46	55%
43.83	10968	31.49		2617	1380.21		7.95	5.04	60%
43.76	12272	37.51		2767	1641.44		7.48	5.67	65%
43.67	13898	45.93		2947	2005.76		6.93	6.50	70%
43.54	15273	55.72		3112	2426.05		6.30	7.44	75%
43.42	16429	66.25		3272	2876.58		5.71	8.40	80%
43.27	18858	78.05		3418	3377.22		5.58	9.44	85%
43.14	21030	90.47		3568	3902.88		5.39	10.45	90%
42.97	22522	102.44		3692	4401.85		5.12	11.39	95%
42.82	23675	114.51		3790	4903.32		4.83	12.36	100%
Load test data						Lithium Battery :12S 48V
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
47.66	6002	11.91		1929	567.63		10.57	2.81	40%
47.61	7651	16.89		1788	804.13		9.51	4.30	45%
47.43	6685	16.33		1975	774.53		8.63	3.75	50%
47.45	11107	29.72		2599	1410.21		7.88	5.18	55%
47.39	12600	35.4		2754	1677.61		7.51	5.82	60%
47.31	14312	43.85		2944	2074.54		6.90	6.73	65%
47.19	16169	52.65		3132	2484.55		6.51	7.58	70%
47.07	17466	62.91		3297	2961.17		5.90	8.58	75%
46.92	19081	74.11		3465	3477.24		5.49	9.58	80%
46.77	21823	88.25		3603	4127.45		5.29	10.94	85%
46.58	23293	101.02		3756	4705.51		4.95	11.96	90%
46.46	25006	114.43		3873	5316.42		4.70	13.11	95%
46.30	26092	126.15		3986	5840.75		4.47	13.99	100%
The above figures are from the actual melting room: sea level requires height, E8-2023 test platform

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Rated power	Max thrust	Max power
UM1115 KV110		150A	F34128 34 inch folding propeller		Multi-rotor drone	12KG-14KG/uniaxial	28.6KG		7330W
Load test data						Lithium Battery :14S 51.8V
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
51.33	5950	12.55		1969	644.19		9.24	3.12	40%
51.25	7410	17.36		2215	889.70		8.33	3.84	45%
51.24	8915	23.02		2435	1179.54		7.56	4.63	50%
51.15	10362	28.23		2613	1443.96		7.18	5.28	55%
51.06	11802	34.79		2812	1776.38		6.64	6.03	60%
50.99	13505	42.31		2995	2157.39		6.26	6.88	65%
50.87	15342	51.07		3189	2597.93		5.91	7.78	70%
50.78	17017	60.74		3386	3084.38		5.52	8.70	75%
50.60	18825	71.84		3560	3635.10		5.18	9.75	80%
50.50	20673	83.52		3727	4217.76		4.90	10.81	85%
50.33	22411	95.48		3906	4805.51		4.66	11.75	90%
50.19	23735	106.99		4056	5369.83		4.42	12.64	95%
50.02	25372	122.17		4224	6110.94		4.15	13.82	100%
Load test data						Lithium Battery :14S 56V
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
55.56	7033	14.63		2132	812.84		8.65	3.64	40%
55.48	8726	20.03		2386	1111.26		7.85	4.45	45%
55.38	10223	25.22		2590	1396.68		7.32	5.15	50%
55.36	11927	32.3		2806	1788.13		6.67	6.09	55%
55.25	13585	39.78		2998	2197.85		6.18	7.00	60%
55.15	16280	48.26		3214	2661.54		6.12	7.91	65%
55.03	17216	59.29		3411	3262.73		5.28	9.13	70%
54.87	19596	70.2		3609	3851.87		5.09	10.19	75%
54.74	21627	80.86		3792	4426.28		4.89	11.15	80%
54.63	23467	93.82		3982	5125.39		4.58	12.29	85%
54.45	25257	106.82		4156	5816.35		4.34	13.37	90%
54.30	26925	119.41		4307	6483.96		4.15	14.38	95%
54.08	28656	135.55		4455	7330.54		3.91	15.71	100%
The above figures are from the actual melting room: sea level requires height, E8-2023 test platform

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Rated power	Max thrust	Max power
UM1115 KV110		150A	F36120 36 inch folding propeller		Multi-rotor drone	12KG-14KG/uniaxial	30.1KG		8385W
Load test data						Lithium Battery :14S 51.8V
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
51.34	6330	13.07		1957	671.01		9.43	3.27	40%
51.26	8048	18.22		2202	933.96		8.62	4.05	45%
51.21	9752	24.23		2410	1240.82		7.86	4.92	50%
51.11	11314	30.27		2594	1547.10		7.31	5.70	55%
51.04	13229	38.19		2787	1949.22		6.79	6.68	60%
50.90	14905	47.14		2976	2399.43		6.21	7.70	65%
50.79	16808	56.3		3154	2859.48		5.88	8.66	70%
50.66	18734	66.98		3331	3393.21		5.52	9.73	75%
50.51	20801	79.05		3498	3992.82		5.21	10.90	80%
50.34	22744	93.74		3655	4718.87		4.82	12.33	85%
50.16	24836	107.11		3787	5372.64		4.62	13.55	90%
50.02	26588	121.84		3901	6094.44		4.36	14.92	95%
49.81	28206	139.22		4010	6934.55		4.07	16.51	100%
Load test data						Lithium Battery :14S 56V
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
55.53	7355	15.02		2104	834.06		8.82	3.79	40%
55.47	9135	20.64		2343	1144.90		7.98	4.67	45%
55.38	10868	26.64		2543	1475.32		7.37	5.54	50%
55.28	12846	33.96		2749	1877.31		6.84	6.52	55%
55.17	14827	43.28		2958	2387.76		6.21	7.71	60%
55.09	16679	51.4		3130	2831.63		5.89	8.64	65%
54.92	18509	61.96		3315	3402.84		5.44	9.80	70%
54.79	20838	74.45		3481	4079.12		5.11	11.19	75%
54.64	22756	87.88		3651	4801.76		4.74	12.56	80%
54.46	24821	101.77		3777	5542.39		4.48	14.01	85%
54.27	26840	117.51		3917	6377.27		4.21	15.55	90%
54.08	28567	133.75		4005	7233.20		3.95	17.25	95%
53.80	30133	155.87		4120	8385.81		3.59	19.44	100%
The above figures are from the actual melting room: sea level requires height, E8-2023 test platform

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Rated power	Max thrust	Max power
UM1115 KV67		150A HV (18S)	G4295 42 inch straight propeller		Multi-rotor drone	10KG-13KG/shaft	1360W	27.8KG	4.6KW
Load test data						Lithium Battery :18S
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
66.98	6034	6.77		1583	453.45		13.3067	2.7356	40%
66.91	7330	9.15		1749	612.23		11.9727	3.3429	45%
66.81	9086	12.06		1944	805.73		11.2768	3.9582	50%
66.69	10859	15.93		2138	1062.37		10.2215	4.7454	55%
66.56	12888	20.52		2303	1365.81		9.4362	5.6637	60%
66.44	14613	24.96		2462	1658.34		8.8118	6.4326	65%
66.27	16702	29.9		2612	1981.47		8.4291	7.2447	70%
66.10	18607	35.95		2757	2376.30		7.8303	8.2313	75%
65.84	20439	42.12		2901	2773.18		7.3702	9.1292	80%
65.63	22498	49.36		3021	3239.50		6.9449	10.2407	85%
65.35	24798	57.93		3165	3785.73		6.5504	11.4230	90%
65.08	26420	65.93		3279	4290.72		6.1575	12.4966	95%
64.90	27841	71.8		3349	4659.82		5.9747	13.2879	100%
The above figures are from the actual melting room: sea level requires height, E8-2023 test platform

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Rated power	Max thrust	Max power
UM1115 KV85		120A	P3812 38 inch straight propeller		Multi-rotor drone	8.0KG-10KG/shaft	1150W	21.9KG	4.1KW
Load test data						Lithium Battery :14S
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
52.93	5310	7.63		1598	403.86		13.1483	2.4135	40%
5287	6461	10.45		1765	552.49		11.6943	2.9894	45%
52.79	7747	13.46		1933	710.55		10.9028	3.5105	50%
52.73	9218	17.54		2101	924.88		9.9667	4.2040	55%
52.63	10723	22.59		2276	1188.91		9.0192	4.9886	60%
52.41	12329	27.4		2440	1436.03		8.5855	5.6205	65%
52.39	13806	34.04		2590	1783.36		7.7416	6.5757	70%
52.11	15372	39.9		2719	2079.19		7.3933	7.3028	75%
51.90	16535	45.73		2854	2373.39		6.9668	7.9418	80%
51.82	18028	52.46		2982	2718.48		6.6317	8.7061	85%
51.54	19688	61.49		3099	3169.19		6.2123	9.7663	90%
51.33	20825	69.68		3216	3576.67		5.8224	10.6210	95%
51.02	21945	81.2		3334	4142.82		5.2971	11.8668	100%
The above figures are from the actual melting room: sea level requires height, E8-2023 test platform

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Rated power	Max thrust	Max power
UM1115 KV85		120A	P4013 40 inch straight propeller		Multi-rotor drone	8.0KG-10KG/shaft	1100W	20.2KG	3.5KW
Load test data						Lithium Battery :12S
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
45.47	4917	7.8		1370	354.67		13.8637	2.4723	40%
45.32	5999	10.54		1519	477.67		12.5588	3.0031	45%
45.18	7224	13.82		1647	62439		11.5697	3.6205	50%
45.18	8352	17.67		1782	798.33		10.4618	4.2784	55%
45.03	9772	22.09		1920	994.71		9.8239	4.9477	60%
44.88	11381	27.45		2053	1231.96		9.2382	5.7307	65%
44.74	12679	33.65		2182	1505.50		8.4218	6.5892	70%
44.51	13914	39.46		2306	1756.36		7.9220	7.2738	75%
44.35	15349	45.8		2414	2031.23		7.5565	8.0357	80%
44.18	17047	52.92		2499	2338.01		7.2913	8.9348	85%
43.98	18542	61.28		2596	2695.09		6.8799	9.9145	90%
43.73	19130	70.43		2690	3079.90		6.2112	10.9342	95%
43.41	20231	80.44		2777	3491.90		5.7937	12.0085	100%
The above figures are from the actual melting room: sea level requires height, E8-2023 test platform

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Rated power	Max thrust	Max power
UM1115 KV85		120A	P4013 40 inch straight propeller		Multi-rotor drone	9.0KG-12KG/shaft	1430W	25.6KG	5.0KW
Load test data						Lithium Battery :14S
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
52.78	6411	10.05		1560	530.44		12.0862	3.2472	40%
52.69	7661	13.19		1720	694.98		11.0233	3.8588	45%
52.61	9347	17.48		1866	919.62		10.1639	4.7065	50%
52.40	10967	21.89		2024	1147.04		9.5612	5.4122	55%
52.54	12440	27.76		2185	1458.51		8.5293	6.3747	60%
52.16	14358	34.25		2333	1786.48		8.0370	7.3129	65%
51.86	16048	41.4		2460	2147.00		7.4746	8.3349	70%
51.70	17656	49.45		2581	2556.57		6.9061	9.4596	75%
51.45	19641	57.63		2680	2965.06		6.6241	10.5658	80%
51.23	21143	66.85		2775	3424.73		6.1736	11.7860	85%
51.08	22389	74.18		2881	3789.11		5.9088	12.5602	90%
50.77	24031	85.59		2958	4345.40		5.5302	14.0293	95%
50.46	25647	100.37		3015	5064.67		5.0639	16.0423	100%
The above figures are from the actual melting room: sea level requires height, E8-2023 test platform

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Rated power	Max thrust	Max power
UM1115 KV95		120A	P3812 38 inch straight propeller		Multi-rotor drone	9.0KG-12KG/shaft	1440W	23.7KG	4.8KW
Load test data						Lithium Battery :14S
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
52.96	6165	9.86		1718	522.19		11.8061	2.9027	40%
5286	7457	13.21		1891	698.28		10.6791	3.5265	45%
52.72	8853	16.93		2072	892.55		9.9188	4.1138	50%
52.62	10385	21.98		2266	1156.59		8.9790	4.8744	55%
52.52	12078	27.43		2442	1440.62		8.3839	5.6339	60%
52.32	13592	34.16		2608	1787.25		7.6050	6.5446	65%
52.13	15597	41.25		2746	2150.36		7.2532	7.4785	70%
52.01	17153	48.54		2884	2524.57		6.7944	8.3598	75%
51.74	18500	56.16		3015	2905.72		6.3668	9.2039	80%
52.02	20044	65.06		3145	3384.42		5.9224	10.2770	85%
51.48	21174	74.16		3254	3817.76		5.5462	11.2045	90%
51.07	22476	82.96		3368	4236.77		5.3050	12.0134	95%
50.64	23793	96.58		3449	4890.81		4.8648	13.5423	100%
60% door working continuously for 15 minutes, motor temperature 89℃, ESC temperature 69℃, ambient temperature 25℃
The above figures are from the actual melting room: sea level requires height, E8-2023 test platform

Power configuration Measured data
Motor		ESC	Propeller		Applicable models	Applicable takeoff weight	Rated power	Max thrust	Max power
UM1115 KV95		120A	P4013 40 inch straight propeller		Multi-rotor drone	9.0KG-11KG/shaft	1200W	22.4KG	4.0KW
Load test data						Lithium Battery :12S
Voltage (V)	Thrust (g)	Current (A)		RPM	Power (W)		Efficiency (g/W)	Torque (N.m)	Throttle
45.27	5757	9.7		1472	439.12		13.1103	2.8489	40%
45.10	6886	12.57		1618	566.91		12.1466	3.3461	45%
45.03	8162	16.67		1758	750.65		10.8732	4.0778	50%
44.89	9615	21.34		1902	957.95		10.0370	4.8099	55%
44.80	11108	27.28		2046	1222.14		9.0889	5.7045	60%
44.64	12679	33.42		2182	1491.87		8.4987	6.5295	65%
44.33	14132	40.3		2312	1786.50		7.9104	7.3794	70%
44.16	15596	47.55		2416	2099.81		7.4273	8.3002	75%
43.95	17060	54.66		2522	2402.31		7.1015	9.0968	80%
43.83	18781	63.92		2608	2801.61		6.7036	10.2590	85%
43.42	20022	73.56		2699	3193.98		6.2687	11.3014	90%
43.40	20984	82.48		2785	3579.63		5.8621	12.2749	95%
42.96	22415	94.04		2857	4039.96		5.5483	13.5042	100%
The above figures are from the actual melting room: sea level requires height, E8-2023 test platform