M8108 UL

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M8108 UL

Industrial Multirotor Drone Motor

Load Performance Parameters:

High Efficiency, Long Endurance

The recommended thrust is

3.5kg+
The efficiency is

12g/w+

The recommended
thrust is

3.5kg

Maximum takeoff weight

12kg

The efficiency is

11g/w

(12S 40Ah)
The takeoff weight

10kg
Flight Time

120minutes

Excellent Design,
New Technology

Industry-level motor technology

has higher speciﬁcations and requires high grade
raw materials, better tolerances, to provide
reliability and performance.
Brand new exterior design,

the hollow shape is more recognizable,
and the coexistence of grandeur
and sophistication.
The new magnetic circuit
design optimizes the
anti-emotive force harmonics,

that produce a higher sine wave and is better
matched with the ESC.

Industry-level motor technology

has higher requirements and stricter control on
incoming materials, process and assembly.
Brand new exterior design,

the hollow shape is more recognizable,
and the coexistence of grandeur
and sophistication.
The new magnetic circuit
design optimizes the
anti-emotive force harmonics,

so that its anti-emotive force is higher sine
and to better matched with the ESC.

Attention to Details,
Extremely Lightweight

The integrated design of the bracket and the rotating shaft
can not only ensure the co-axiality of the stator and rotor,
but also reduce the number of parts and simplify the process.
The tail of the main shaft uses three M2.5*8 and
washer locking designs to enhance motor reliability.

The integrated design of the bracket and the rotating shaft
can not only ensure the co-axiality of the stator and rotor,
but also reduce the number of parts and simplify the process.
The tail of the spindle shaft uses three M2.5*8 and
washer locking designs to enhance motor reliability.

Adopts High
Quality Materials,
Safe and Reliable

Made of solid materials to improve durability and provide
reliable guarantee for motor performance.

High-quality bearings

and low friction torque effectively
extend the lifespan of the motor.
High-strength aviation aluminum

7075
PrecisionCNC
machined rotor bracket
The outer rotor casing is made of

20# seamless steel rotor with nickel
electrophoresis design, which has excellent
magnetic permeability
and corrosion resistance.
16AWG

highly ﬂexible silicone wire,
low resistivity and good toughness
High-performance iron core punched from

0.2mmlow-loss silicon steel sheet

Recommended
Combinations

Motor
M8108 UL
Battery
12S LiPo/6S LiPo
Propeller
GP28×9.2"/GP29×9.5"/ML30*9.8"
Thrust/rotor
2.5~3.5kg
ESC
XRotor Pro-H60A-14S
Takeoff weight of quadrotor
10.0~14.0kg

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M8108 UL CAD

Model

M8108 UL 85KV

M8108 UL 100KV

M108 UL 150KV

Specification

Motor Size	Φ87.1*H25.4mm	Φ87.1*H25.4mm	Φ87.1*H25.4mm
Stator Size	Φ81mm	Φ81mm	Φ81mm
Stator process	High standard silicon steel sheet, rust proof, 180℃ high temperature resistance paint-coat	High standard silicon steel sheet, rust proof, 180℃ high temperature resistance paint-coat	High standard silicon steel sheet, rust proof, 180℃ high temperature resistance paint-coat
Enamelled wire	200℃	200℃	200℃
Magnet	180℃	180℃	180℃
Isolation test	500V AC high voltage resistance test	500V AC high voltage resistance test	500V AC high voltage resistance test
Protection level	IPX5	IPX5	IPX5
Slot& Pole	36N 42P	36N 42P	36N 42P
Dynamic balance	≤10mg	≤10mg	≤10mg
Bearing	Water proof bearing	Water proof bearing	Water proof bearing
Motor axle diameter	/	/	/
Props mounting dimensions	4×M3@D20mm+4×M4@D23mm	4×M3@D20mm+4×M4@D23mm	4×M3@D20mm+4×M4@D23mm
Motor mounting dimensions	4×M4@D36mm	4×M4@D36mm	4×M4@D36mm
KV	85	100	150
Battery(LiPo)	12S LiPo	12S LiPo	6S LiPo
No-load current	0.91A	1.19A	1.41A
Maximum current (Non-hermetic Ambient Temperature ≤ 25℃）	20.8A	33.8A	27.8A
Max power	950W	1550W	640W
Max thrust	7.2kg	9.2kg	5.5kg
Resistance	239.5 mΩ	165.2 mΩ	82.8 mΩ
Wire Size	16 AWG	16 AWG	16 AWG
Wire length	100 mm	100 mm	100 mm
Weight（With wire）	237.4g	238.3g	242.8g
Rated power input	330W	330W	330W
Rated power output	280.5W	280.5W	280.5W

Recommended Combinations

Motor	M8108 UL 85KV	M8108 UL 100KV	M8108 UL 150KV
Propeller	289.2"/299.5"/30*9.8"	289.2"/299.5"/30*9.8"	289.2"/299.5"/30*9.8"
ESC	XRotor Pro-H60A-14S	XRotor Pro-H60A-14S	XRotor Pro-H60A-14S
Battery	12S LiPo	12S LiPo	6S LiPo
Thrust/rotor	2.5~3.5kg	2.5~3.5kg	2.5~3.5kg
Takeoff weight of quadrotor	10~14kg	10~14kg	10~14kg

M8108 UL 85KV+GP29*9.5" Load performance parameters

M8108 UL 85KV+GP29*9.5"Motor Propeller Thrust Test Data

Voltage(V)	Propeller	Throttle(%)	Thrust(g)	Current(A)	Power Input(W)	Speed(RPM)	Efficiency(g/W)	Torque(N·m)	Power Output(W)	Temperature(℃)
46V (12S LiPo)	GP29*9.5"	33%	1171	1.5	69.6	1270	16.8	0.41	59.2	66.1°C
		35%	1285	1.7	78.6	1331	16.3	0.45	66.8
		37%	1413	1.9	89.4	1398	15.8	0.49	76.0
		39%	1552	2.2	101.9	1467	15.2	0.54	86.6
		42%	1778	2.7	123.7	1575	14.4	0.62	105.1
		45%	2021	3.2	148.8	1683	13.6	0.70	126.5
		48%	2279	3.8	176.9	1789	12.9	0.79	150.4
		51%	2549	4.5	207.6	1891	12.3	0.88	176.5
		54%	2828	5.2	240.8	1989	11.7	0.97	204.7
		57%	3117	6.0	276.4	2083	11.3	1.06	235.0
		60%	3412	6.8	314.6	2172	10.8	1.16	267.4
		63%	3715	7.7	355.5	2259	10.5	1.26	302.2
		66%	4024	8.7	399.5	2344	10.1	1.36	339.5
		69%	4339	9.7	446.8	2428	9.7	1.47	379.8
		72%	4657	10.8	497.7	2512	9.4	1.58	423.1
		75%	4977	12.0	552.1	2596	9.0	1.69	469.3
		78%	5296	13.2	609.5	2680	8.7	1.80	518.1
		81%	5611	14.5	669.0	2763	8.4	1.91	568.7
		84%	5917	15.8	729.0	2843	8.1	2.01	619.7
		87%	6208	17.1	787.3	2916	7.9	2.11	669.2
		90%	6476	18.3	841.4	2979	7.7	2.20	715.2
		100%	7060	20.7	954.7	3092	7.4	2.37	811.5

以上数据为好盈实验室于室温 25℃、海平面高度，变化Throttle输入调节测得，Temperature为65%Throttle运行10分钟数据，仅供参考。

M8108 UL 85KV+ML30*9.8" Load performance parameters

M8108 UL 85KV+ML30*9.8" Motor Propeller Thrust Test Data

Voltage(V)	Propeller	Throttle(%)	Thrust(g)	Current(A)	Power Input(W)	Speed(RPM)	Efficiency(g/W)	Torque(N·m)	Power Output(W)	Temperature(℃)
46V (12S LiPo)	ML30*9.8"	33%	1164	1.5	68.2	1269	17.1	0.40	58.0	69.2°C
		35%	1274	1.7	76.7	1330	16.6	0.43	65.2
		37%	1402	1.9	87.2	1397	16.1	0.48	74.2
		39%	1545	2.2	99.6	1468	15.5	0.52	84.7
		42%	1780	2.6	121.4	1578	14.7	0.60	103.2
		45%	2035	3.2	146.4	1688	13.9	0.69	124.5
		48%	2302	3.8	174.2	1794	13.2	0.77	148.1
		51%	2578	4.4	204.4	1895	12.6	0.86	173.7
		54%	2861	5.1	236.7	1993	12.1	0.95	201.2
		57%	3149	5.9	271.1	2087	11.6	1.04	230.4
		60%	3443	6.7	307.8	2178	11.2	1.14	261.6
		63%	3741	7.5	347.0	2267	10.8	1.23	294.9
		66%	4044	8.5	389.2	2355	10.4	1.33	330.8
		69%	4353	9.4	434.7	2442	10.0	1.43	369.5
		72%	4668	10.5	484.0	2529	9.6	1.53	411.4
		75%	4988	11.7	537.0	2615	9.3	1.64	456.4
		78%	5312	12.9	593.5	2699	8.9	1.75	504.5
		81%	5636	14.2	652.9	2781	8.6	1.86	554.9
		84%	5958	15.5	713.5	2857	8.4	1.97	606.5
		87%	6271	16.8	773.3	2927	8.1	2.07	657.3
		90%	6567	18.0	829.3	2988	7.9	2.17	704.9
		100%	7258	20.6	949.1	3102	7.6	2.36	806.8

The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, the motor temperature is 65% and the throttle runs for 10 minutes, for reference only.

M8108 UL 100KV+GP28*9.2" Load performance parameters

M8108 UL 100KV+GP28*9.2"Motor Propeller Thrust Test Data

Voltage(V)	Propeller	Throttle(%)	Thrust(g)	Current(A)	Power Input(W)	Speed(RPM)	Efficiency(g/W)	Torque(N·m)	Power Output(W)	Temperature(℃)
46V(12S LiPo)	GP28*9.2"	33%	1438	2.1	97.8	1508	14.7	0.46	83.1	73.2°C
		35%	1599	2.4	111.7	1587	14.3	0.52	94.9
		37%	1778	2.8	128.5	1672	13.8	0.57	109.2
		39%	1972	3.2	147.9	1760	13.3	0.64	125.7
		42%	2281	3.9	181.4	1894	12.6	0.74	154.2
		45%	2605	4.8	219.3	2024	11.9	0.84	186.4
		48%	2937	5.7	260.7	2149	11.3	0.95	221.6
		51%	3273	6.6	305.0	2268	10.7	1.05	259.2
		54%	3613	7.6	351.9	2381	10.3	1.16	299.1
		57%	3955	8.7	401.4	2488	9.9	1.27	341.2
		60%	4301	9.9	454.0	2592	9.5	1.38	385.9
		63%	4654	11.1	510.2	2692	9.1	1.49	433.7
		66%	5014	12.4	570.7	2791	8.8	1.60	485.1
		69%	5383	13.8	636.1	2890	8.5	1.72	540.7
		72%	5763	15.4	707.4	2988	8.1	1.84	601.3
		75%	6151	17.1	784.7	3087	7.8	1.97	667.0
		78%	6547	18.9	868.1	3185	7.5	2.10	737.9
		81%	6946	20.8	956.6	3282	7.3	2.24	813.1
		84%	7338	22.8	1048.2	3373	7.0	2.37	890.9
		87%	7714	24.8	1139.2	3458	6.8	2.50	968.3
		90%	8059	26.6	1224.7	3530	6.6	2.61	1041.0
		100%	8693	30.1	1384.4	3647	6.3	2.81	1176.7

M8108 UL 100KV+GP29*9.5" Load performance parameters

M8108 UL 100KV+GP29*9.5" Motor Propeller Thrust Test Data

Voltage(V)	Propeller	Throttle(%)	Thrust(g)	Current(A)	Power Input(W)	Speed(RPM)	Efficiency(g/W)	Torque(N·m)	Power Output(W)	Temperature(℃)
46V(12S LiPo)	GP29*9.5"	33%	1611	2.4	110.7	1486	14.5	0.54	94.1	77.4°C
		35%	1795	2.8	127.4	1566	14.1	0.61	108.3
		37%	1994	3.2	146.9	1649	13.6	0.67	124.9
		39%	2205	3.7	169.0	1734	13.0	0.74	143.6
		42%	2537	4.5	206.6	1862	12.3	0.85	175.6
		45%	2884	5.4	249.1	1987	11.6	0.97	211.8
		48%	3241	6.4	295.8	2106	11.0	1.09	251.5
		51%	3604	7.5	346.3	2219	10.4	1.21	294.4
		54%	3972	8.7	400.3	2326	9.9	1.34	340.3
		57%	4344	9.9	457.8	2427	9.5	1.46	389.1
		60%	4720	11.3	518.8	2524	9.1	1.59	441.0
		63%	5101	12.7	583.8	2617	8.7	1.72	496.2
		66%	5487	14.2	653.1	2709	8.4	1.85	555.1
		69%	5878	15.8	727.1	2801	8.1	1.98	618.0
		72%	6273	17.5	806.2	2892	7.8	2.11	685.3
		75%	6670	19.4	890.6	2984	7.5	2.24	757.0
		78%	7068	21.3	980.1	3076	7.2	2.38	833.1
		81%	7461	23.3	1073.9	3165	6.9	2.51	912.8
		84%	7842	25.4	1170.4	3249	6.7	2.64	994.9
		87%	8204	27.5	1267.1	3324	6.5	2.77	1077.0
		90%	8533	29.6	1359.8	3387	6.3	2.88	1155.8
		100%	9187	33.8	1556.3	3480	5.9	3.11	1322.9

M8108 UL 150KV+GP28*9.2" Load performance parameters

M8108 UL 150KV+GP28*9.2" Motor Propeller Thrust Test Data

Voltage(V)	Propeller	Throttle(%)	Thrust(g)	Current(A)	Power Input(W)	Speed(RPM)	Efficiency(g/W)	Torque(N·m)	Power Output(W)	Temperature(℃)
23V(6S LiPo)	GP28*9.2"	33%	871	2.0	47.2	1096	18.5	0.30	40.1	54.2°C
		35%	968	2.3	53.7	1151	18.0	0.33	45.7
		37%	1070	2.7	61.2	1207	17.5	0.37	52.0
		39%	1178	3.0	69.5	1266	16.9	0.40	59.1
		42%	1349	3.6	83.6	1355	16.1	0.46	71.1
		45%	1529	4.3	99.6	1445	15.4	0.52	84.7
		48%	1720	5.1	117.4	1535	14.6	0.59	99.8
		51%	1919	5.9	137.0	1623	14.0	0.66	116.4
		54%	2127	6.9	158.4	1709	13.4	0.72	134.6
		57%	2344	7.9	181.6	1793	12.9	0.80	154.3
		60%	2569	9.0	206.7	1875	12.4	0.87	175.7
		63%	2802	10.1	234.0	1954	12.0	0.95	198.9
		66%	3043	11.4	263.5	2032	11.5	1.03	224.0
		69%	3290	12.8	295.3	2109	11.1	1.11	251.0
		72%	3542	14.3	329.6	2185	10.7	1.19	280.2
		75%	3798	15.9	366.3	2262	10.4	1.28	311.3
		78%	4054	17.6	404.9	2339	10.0	1.37	344.2
		81%	4307	19.3	445.0	2414	9.7	1.46	378.2
		84%	4554	21.0	485.3	2487	9.4	1.54	412.5
		87%	4789	22.8	524.7	2554	9.1	1.62	446.0
		90%	5005	24.3	561.3	2611	8.9	1.70	477.1
		100%	5483	27.8	640.0	2712	8.6	1.84	544.0

M8108 UL 150KV+GP29*9.5" Load performance parameters

M8108 UL 150KV+GP29*9.5" Motor Propeller Thrust Test Data

Voltage(V)	Propeller	Throttle(%)	Thrust(g)	Current(A)	Power Input(W)	Speed(RPM)	Efficiency(g/W)	Torque(N·m)	Power Output(W)	Temperature(℃)
23V(6S LiPo)	GP29*9.5"	33%	869	2.0	46.1	1096	18.9	0.30	39.2	53.6°C
		35%	963	2.3	52.4	1151	18.4	0.33	44.5
		37%	1064	2.6	59.6	1208	17.8	0.36	50.7
		39%	1171	2.9	67.8	1266	17.3	0.40	57.6
		42%	1341	3.5	81.7	1356	16.4	0.45	69.5
		45%	1522	4.2	97.6	1447	15.6	0.51	82.9
		48%	1712	5.0	115.2	1537	14.9	0.58	97.9
		51%	1911	5.8	134.4	1625	14.2	0.64	114.3
		54%	2117	6.7	155.4	1711	13.6	0.71	132.1
		57%	2332	7.7	178.1	1796	13.1	0.78	151.4
		60%	2555	8.8	202.5	1878	12.6	0.85	172.1
		63%	2786	9.9	228.9	1958	12.2	0.93	194.6
		66%	3026	11.2	257.4	2037	11.8	1.00	218.8
		69%	3273	12.5	288.2	2115	11.4	1.08	245.0
		72%	3528	13.9	321.4	2193	11.0	1.17	273.2
		75%	3788	15.5	356.9	2269	10.6	1.25	303.4
		78%	4050	17.1	394.7	2345	10.3	1.34	335.5
		81%	4312	18.8	434.1	2419	9.9	1.42	369.0
		84%	4569	20.6	474.2	2490	9.6	1.51	403.1
		87%	4814	22.3	513.8	2556	9.4	1.59	436.8
		90%	5040	23.9	551.1	2615	9.1	1.66	468.4
		100%	5517	27.3	629.8	2726	8.8	1.82	535.4

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M8108 UL Specification

M8108 UL Load performance parameters

M8108 UL 3D Model Drawing

M8108 UL CAD

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M8108 UL

Industrial Multirotor Drone Motor

LOAD PERFORMANCE PARAMETERS:

High Efficiency, Long Endurance

The recommended
thrust is

3.5kg+
The efficiency is

11g/w+

The recommended thrust is

3.5kg

Takeoff weight of quadrotor

12kg

The efficiency is

11g/w

(12S 40Ah)
The takeoff weight

10kg
Flight Time

120minutes

Excellent Design,
New Technology

Industry-level motor technology

has higher requirements and stricter control
on incoming materials, process and assembly.
Brand new exterior design,

optimized fan ports effectively
improve the protection level.
he new magnetic circuit design
optimizes the anti-emotive force harmonics,

so that its anti-emotive force is higher sine
and to better matched with the ESC.

Industry-level motor technology

has higher requirements and stricter control
on incoming materials, process and assembly.
Brand new exterior design,

the hollow shape is more recognizable,
and the coexistence of grandeur
and sophistication.
The new magnetic circuit
design optimizes the
anti-emotive force harmonics,

so that its anti-emotive force is higher sine
and to better matched with the ESC.

Attention to Details, Extremely Lightweight

Adopts a fully enclosed structure,
the protection level reaches IP54.
The integrated design of the bracket
and the rotating shaft can not only
ensure the co-axiality of the stator
and rotor, but also reduce the number
of parts and simplify the process.
The rotor bracket is equipped with a
high-efﬁciency centrifugal air-cooling
system, and the stator base has built-in
large-area heat sinks to effectively
improve heat dissipation capacity.
The tail of the spindle shaft uses three
M2.5*8 and washer locking designs to
enhance motor reliability.

The integrated design of the bracket and
the rotating shaft can not only ensure
the co-axiality of the stator and rotor,
but also reduce the number of parts
and simplify the process.
The tail of the spindle shaft uses three
M2.5*8 and washer locking designs to
enhance motor reliability.

Adopts High
Quality Materials,
Safe and Reliable

Made of solid materials to improve durability and
provide reliable guarantee for motor performance.

The outer rotor casing is made of 20# seamless steel tube with nickel electrophoresis design, which has excellent magnetic permeability and corrosion resistance.
High-quality bearingsand low friction torque effectively extend the lifespan of the motor.
Precision CNC machined rotor bracket High-strength aviation aluminum 7075
16AWG highly ﬂexible silicone wire, low resistivity and good toughness
High-performance iron core punched from 0.2mm low-loss silicon steel sheet

Recommended
Combinations

Motor
M8108 UL
Battery
12S LiPo/6S LiPo
Propeller
GP28×9.2"
GP29×9.5"
ML30*9.8"
Takeoff weight/rotor
2.5~3.5kg
ESC
XRotor Pro-H60A-14S
Takeoff weight of quadrotor
10.0~14.0kg

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M8108 UL CAD

Model

M8108 UL 85KV

M8108 UL 100KV

M108 UL 150KV

Specification

Motor Size	Φ87.1*H25.4mm	Φ87.1*H25.4mm	Φ87.1*H25.4mm
Stator Size	Φ81mm	Φ81mm	Φ81mm
Stator process	High standard silicon steel sheet, rust proof, 180℃ high temperature resistance paint-coat	High standard silicon steel sheet, rust proof, 180℃ high temperature resistance paint-coat	High standard silicon steel sheet, rust proof, 180℃ high temperature resistance paint-coat
Enamelled wire	200℃	200℃	200℃
Magnet	180℃	180℃	180℃
Isolation test	500V AC high voltage resistance test	500V AC high voltage resistance test	500V AC high voltage resistance test
Protection level	IPX5	IPX5	IPX5
Slot& Pole	36N 42P	36N 42P	36N 42P
Dynamic balance	≤10mg	≤10mg	≤10mg
Bearing	Water proof bearing	Water proof bearing	Water proof bearing
Motor axle diameter	/	/	/
Props mounting dimensions	4×M3@D20mm+4×M4@D23mm	4×M3@D20mm+4×M4@D23mm	4×M3@D20mm+4×M4@D23mm
Motor mounting dimensions	4×M4@D36mm	4×M4@D36mm	4×M4@D36mm
KV	85	100	150
Battery(LiPo)	12S LiPo	12S LiPo	6S LiPo
No-load current	0.91A	1.19A	1.41A
Maximum current (Non-hermetic Ambient Temperature ≤ 25℃）	20.8A	33.8A	27.8A
Max power	950W	1550W	640W
Max thrust	7.2kg	9.2kg	5.5kg
Resistance	239.5 mΩ	165.2 mΩ	82.8 mΩ
Wire Size	16 AWG	16 AWG	16 AWG
Wire length	100 mm	100 mm	100 mm
Weight（With wire）	237.4g	238.3g	242.8g
Rated power input	330W	330W	330W
Rated power output	280.5W	280.5W	280.5W

Recommended Combinations

Motor	M8108 UL 85KV	M8108 UL 100KV	M8108 UL 150KV
Propeller	289.2"/299.5"/30*9.8"	289.2"/299.5"/30*9.8"	289.2"/299.5"/30*9.8"
ESC	XRotor Pro-H60A-14S	XRotor Pro-H60A-14S	XRotor Pro-H60A-14S
Battery	12S LiPo	12S LiPo	6S LiPo
Thrust/rotor	2.5~3.5kg	2.5~3.5kg	2.5~3.5kg
Takeoff weight of quadrotor	10~14kg	10~14kg	10~14kg

M8108 UL 85KV+GP29*9.5" Load performance parameters

M8108 UL 85KV+GP29*9.5"Motor Propeller Thrust Test Data

Voltage(V)	Propeller	Throttle(%)	Thrust(g)	Current(A)	Power Input(W)	Speed(RPM)	Efficiency(g/W)	Torque(N·m)	Power Output(W)	Temperature(℃)
46V (12S LiPo)	GP29*9.5"	33%	1171	1.5	69.6	1270	16.8	0.41	59.2	66.1°C
		35%	1285	1.7	78.6	1331	16.3	0.45	66.8
		37%	1413	1.9	89.4	1398	15.8	0.49	76.0
		39%	1552	2.2	101.9	1467	15.2	0.54	86.6
		42%	1778	2.7	123.7	1575	14.4	0.62	105.1
		45%	2021	3.2	148.8	1683	13.6	0.70	126.5
		48%	2279	3.8	176.9	1789	12.9	0.79	150.4
		51%	2549	4.5	207.6	1891	12.3	0.88	176.5
		54%	2828	5.2	240.8	1989	11.7	0.97	204.7
		57%	3117	6.0	276.4	2083	11.3	1.06	235.0
		60%	3412	6.8	314.6	2172	10.8	1.16	267.4
		63%	3715	7.7	355.5	2259	10.5	1.26	302.2
		66%	4024	8.7	399.5	2344	10.1	1.36	339.5
		69%	4339	9.7	446.8	2428	9.7	1.47	379.8
		72%	4657	10.8	497.7	2512	9.4	1.58	423.1
		75%	4977	12.0	552.1	2596	9.0	1.69	469.3
		78%	5296	13.2	609.5	2680	8.7	1.80	518.1
		81%	5611	14.5	669.0	2763	8.4	1.91	568.7
		84%	5917	15.8	729.0	2843	8.1	2.01	619.7
		87%	6208	17.1	787.3	2916	7.9	2.11	669.2
		90%	6476	18.3	841.4	2979	7.7	2.20	715.2
		100%	7060	20.7	954.7	3092	7.4	2.37	811.5

以上数据为好盈实验室于室温 25℃、海平面高度，变化Throttle输入调节测得，Temperature为65%Throttle运行10分钟数据，仅供参考。

M8108 UL 85KV+ML30*9.8" Load performance parameters

M8108 UL 85KV+ML30*9.8" Motor Propeller Thrust Test Data

Voltage(V)	Propeller	Throttle(%)	Thrust(g)	Current(A)	Power Input(W)	Speed(RPM)	Efficiency(g/W)	Torque(N·m)	Power Output(W)	Temperature(℃)
46V (12S LiPo)	ML30*9.8"	33%	1164	1.5	68.2	1269	17.1	0.40	58.0	69.2°C
		35%	1274	1.7	76.7	1330	16.6	0.43	65.2
		37%	1402	1.9	87.2	1397	16.1	0.48	74.2
		39%	1545	2.2	99.6	1468	15.5	0.52	84.7
		42%	1780	2.6	121.4	1578	14.7	0.60	103.2
		45%	2035	3.2	146.4	1688	13.9	0.69	124.5
		48%	2302	3.8	174.2	1794	13.2	0.77	148.1
		51%	2578	4.4	204.4	1895	12.6	0.86	173.7
		54%	2861	5.1	236.7	1993	12.1	0.95	201.2
		57%	3149	5.9	271.1	2087	11.6	1.04	230.4
		60%	3443	6.7	307.8	2178	11.2	1.14	261.6
		63%	3741	7.5	347.0	2267	10.8	1.23	294.9
		66%	4044	8.5	389.2	2355	10.4	1.33	330.8
		69%	4353	9.4	434.7	2442	10.0	1.43	369.5
		72%	4668	10.5	484.0	2529	9.6	1.53	411.4
		75%	4988	11.7	537.0	2615	9.3	1.64	456.4
		78%	5312	12.9	593.5	2699	8.9	1.75	504.5
		81%	5636	14.2	652.9	2781	8.6	1.86	554.9
		84%	5958	15.5	713.5	2857	8.4	1.97	606.5
		87%	6271	16.8	773.3	2927	8.1	2.07	657.3
		90%	6567	18.0	829.3	2988	7.9	2.17	704.9
		100%	7258	20.6	949.1	3102	7.6	2.36	806.8

M8108 UL 100KV+GP28*9.2" Load performance parameters

M8108 UL 100KV+GP28*9.2"Motor Propeller Thrust Test Data

Voltage(V)	Propeller	Throttle(%)	Thrust(g)	Current(A)	Power Input(W)	Speed(RPM)	Efficiency(g/W)	Torque(N·m)	Power Output(W)	Temperature(℃)
46V(12S LiPo)	GP28*9.2"	33%	1438	2.1	97.8	1508	14.7	0.46	83.1	73.2°C
		35%	1599	2.4	111.7	1587	14.3	0.52	94.9
		37%	1778	2.8	128.5	1672	13.8	0.57	109.2
		39%	1972	3.2	147.9	1760	13.3	0.64	125.7
		42%	2281	3.9	181.4	1894	12.6	0.74	154.2
		45%	2605	4.8	219.3	2024	11.9	0.84	186.4
		48%	2937	5.7	260.7	2149	11.3	0.95	221.6
		51%	3273	6.6	305.0	2268	10.7	1.05	259.2
		54%	3613	7.6	351.9	2381	10.3	1.16	299.1
		57%	3955	8.7	401.4	2488	9.9	1.27	341.2
		60%	4301	9.9	454.0	2592	9.5	1.38	385.9
		63%	4654	11.1	510.2	2692	9.1	1.49	433.7
		66%	5014	12.4	570.7	2791	8.8	1.60	485.1
		69%	5383	13.8	636.1	2890	8.5	1.72	540.7
		72%	5763	15.4	707.4	2988	8.1	1.84	601.3
		75%	6151	17.1	784.7	3087	7.8	1.97	667.0
		78%	6547	18.9	868.1	3185	7.5	2.10	737.9
		81%	6946	20.8	956.6	3282	7.3	2.24	813.1
		84%	7338	22.8	1048.2	3373	7.0	2.37	890.9
		87%	7714	24.8	1139.2	3458	6.8	2.50	968.3
		90%	8059	26.6	1224.7	3530	6.6	2.61	1041.0
		100%	8693	30.1	1384.4	3647	6.3	2.81	1176.7

M8108 UL 100KV+GP29*9.5" Load performance parameters

M8108 UL 100KV+GP29*9.5" Motor Propeller Thrust Test Data

Voltage(V)	Propeller	Throttle(%)	Thrust(g)	Current(A)	Power Input(W)	Speed(RPM)	Efficiency(g/W)	Torque(N·m)	Power Output(W)	Temperature(℃)
46V(12S LiPo)	GP29*9.5"	33%	1611	2.4	110.7	1486	14.5	0.54	94.1	77.4°C
		35%	1795	2.8	127.4	1566	14.1	0.61	108.3
		37%	1994	3.2	146.9	1649	13.6	0.67	124.9
		39%	2205	3.7	169.0	1734	13.0	0.74	143.6
		42%	2537	4.5	206.6	1862	12.3	0.85	175.6
		45%	2884	5.4	249.1	1987	11.6	0.97	211.8
		48%	3241	6.4	295.8	2106	11.0	1.09	251.5
		51%	3604	7.5	346.3	2219	10.4	1.21	294.4
		54%	3972	8.7	400.3	2326	9.9	1.34	340.3
		57%	4344	9.9	457.8	2427	9.5	1.46	389.1
		60%	4720	11.3	518.8	2524	9.1	1.59	441.0
		63%	5101	12.7	583.8	2617	8.7	1.72	496.2
		66%	5487	14.2	653.1	2709	8.4	1.85	555.1
		69%	5878	15.8	727.1	2801	8.1	1.98	618.0
		72%	6273	17.5	806.2	2892	7.8	2.11	685.3
		75%	6670	19.4	890.6	2984	7.5	2.24	757.0
		78%	7068	21.3	980.1	3076	7.2	2.38	833.1
		81%	7461	23.3	1073.9	3165	6.9	2.51	912.8
		84%	7842	25.4	1170.4	3249	6.7	2.64	994.9
		87%	8204	27.5	1267.1	3324	6.5	2.77	1077.0
		90%	8533	29.6	1359.8	3387	6.3	2.88	1155.8
		100%	9187	33.8	1556.3	3480	5.9	3.11	1322.9

M8108 UL 150KV+GP28*9.2" Load performance parameters

M8108 UL 150KV+GP28*9.2" Motor Propeller Thrust Test Data

Voltage(V)	Propeller	Throttle(%)	Thrust(g)	Current(A)	Power Input(W)	Speed(RPM)	Efficiency(g/W)	Torque(N·m)	Power Output(W)	Temperature(℃)
23V(6S LiPo)	GP28*9.2"	33%	871	2.0	47.2	1096	18.5	0.30	40.1	54.2°C
		35%	968	2.3	53.7	1151	18.0	0.33	45.7
		37%	1070	2.7	61.2	1207	17.5	0.37	52.0
		39%	1178	3.0	69.5	1266	16.9	0.40	59.1
		42%	1349	3.6	83.6	1355	16.1	0.46	71.1
		45%	1529	4.3	99.6	1445	15.4	0.52	84.7
		48%	1720	5.1	117.4	1535	14.6	0.59	99.8
		51%	1919	5.9	137.0	1623	14.0	0.66	116.4
		54%	2127	6.9	158.4	1709	13.4	0.72	134.6
		57%	2344	7.9	181.6	1793	12.9	0.80	154.3
		60%	2569	9.0	206.7	1875	12.4	0.87	175.7
		63%	2802	10.1	234.0	1954	12.0	0.95	198.9
		66%	3043	11.4	263.5	2032	11.5	1.03	224.0
		69%	3290	12.8	295.3	2109	11.1	1.11	251.0
		72%	3542	14.3	329.6	2185	10.7	1.19	280.2
		75%	3798	15.9	366.3	2262	10.4	1.28	311.3
		78%	4054	17.6	404.9	2339	10.0	1.37	344.2
		81%	4307	19.3	445.0	2414	9.7	1.46	378.2
		84%	4554	21.0	485.3	2487	9.4	1.54	412.5
		87%	4789	22.8	524.7	2554	9.1	1.62	446.0
		90%	5005	24.3	561.3	2611	8.9	1.70	477.1
		100%	5483	27.8	640.0	2712	8.6	1.84	544.0

M8108 UL 150KV+GP29*9.5" Load performance parameters

M8108 UL 150KV+GP29*9.5" Motor Propeller Thrust Test Data

Voltage(V)	Propeller	Throttle(%)	Thrust(g)	Current(A)	Power Input(W)	Speed(RPM)	Efficiency(g/W)	Torque(N·m)	Power Output(W)	Temperature(℃)
23V(6S LiPo)	GP29*9.5"	33%	869	2.0	46.1	1096	18.9	0.30	39.2	53.6°C
		35%	963	2.3	52.4	1151	18.4	0.33	44.5
		37%	1064	2.6	59.6	1208	17.8	0.36	50.7
		39%	1171	2.9	67.8	1266	17.3	0.40	57.6
		42%	1341	3.5	81.7	1356	16.4	0.45	69.5
		45%	1522	4.2	97.6	1447	15.6	0.51	82.9
		48%	1712	5.0	115.2	1537	14.9	0.58	97.9
		51%	1911	5.8	134.4	1625	14.2	0.64	114.3
		54%	2117	6.7	155.4	1711	13.6	0.71	132.1
		57%	2332	7.7	178.1	1796	13.1	0.78	151.4
		60%	2555	8.8	202.5	1878	12.6	0.85	172.1
		63%	2786	9.9	228.9	1958	12.2	0.93	194.6
		66%	3026	11.2	257.4	2037	11.8	1.00	218.8
		69%	3273	12.5	288.2	2115	11.4	1.08	245.0
		72%	3528	13.9	321.4	2193	11.0	1.17	273.2
		75%	3788	15.5	356.9	2269	10.6	1.25	303.4
		78%	4050	17.1	394.7	2345	10.3	1.34	335.5
		81%	4312	18.8	434.1	2419	9.9	1.42	369.0
		84%	4569	20.6	474.2	2490	9.6	1.51	403.1
		87%	4814	22.3	513.8	2556	9.4	1.59	436.8
		90%	5040	23.9	551.1	2615	9.1	1.66	468.4
		100%	5517	27.3	629.8	2726	8.8	1.82	535.4

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