M 8108/8110 UL
Buy
HM 8108 / 8110 UL
Industrial Multirotor Drone Motors
Load Performance Parameters:
HM8108 HM8110
High Efficiency, Long Endurance
  • The recommended thrust is
    3kg+
  • The efficiency is
    12g/w+
The recommended
thrust is
3kg
Maximum takeoff weight
12kg
The efficiency is
11g/w
  • (12S 40Ah)
  • The takeoff weight
    10kg
  • The endurance
    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
    HM 8108 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
  • Motor
    HM 8110 UL
    Battery
    12S LiPo                  
  • Propeller
    GP29×9.5"/ML30*9.8"/GP32×10.5"
    Thrust/rotor
    3.0~4.0kg
  • ESC
    XRotor Pro-H60A-14S
    Takeoff weight of quadrotor
    12.0~16.0kg
M 8108 UL CAD
M 8110 UL CAD
Model
M 8108 85KV UL M 8108 100KV UL M 8108 150KV UL M 8110 95KV UL M 8110 110KV UL
Specification
Motor Size Φ87.1*H25.4mm Φ87.1*H25.4mm Φ87.1*H25.4mm Φ87.1*H27.4mm Φ87.1*H27.4mm
Stator Size Φ81mm Φ81mm 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 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℃ 200℃ 200℃
Magnet 180℃ 180℃ 180℃ 180℃ 180℃
Isolation test 500V AC high voltage resistance test 500V AC high voltage resistance test 500V AC high voltage resistance test 500V AC high voltage resistance test 500V AC high voltage resistance test
Protection level IPX5 IPX5 IPX5 IPX5 IPX5
Slot& Pole 36N 42P 36N 42P 36N 42P 36N 42P 36N 42P
Dynamic balance ≤10mg ≤10mg ≤10mg ≤10mg ≤10mg
Bearing Water proof bearing Water proof 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 4×M3@D20mm+4×M4@D23mm 4×M3@D20mm+4×M4@D23mm
Motor mounting dimensions 4×M4@D36mm 4×M4@D36mm 4×M4@D36mm 4×M4@D36mm 4×M4@D36mm
KV 85 100 150 95 110
Battery(LiPo) 12S LiPo 12S LiPo 6S LiPo 12S LiPo 12S LiPo
No-load current 0.91A 1.19A 1.41A 1.1A 1.27A
Maximum current (Non-hermetic Ambient Temperature ≤ 25℃） 20.8A 33.8A 27.8A 43.3A 39.2A
Max power 950W 1550W 640W 2000W 1800W
Max thrust 7.2kg 9.2kg 5.5kg 11.4kg 11.1kg
Resistance 239.5 mΩ 165.2 mΩ 82.8 mΩ 132.9 mΩ 112.3 mΩ
Wire Size 16 AWG 16 AWG 16 AWG 16 AWG 16 AWG
Wire length 100 mm 100 mm 100 mm 100 mm 100 mm
Weight（With wire） 237.4g 238.3g 242.8g 300.5g 301.5g
Recommended application combinations
Motor M-8108-UL-85KV M-8108-UL-100KV M-8108-UL-150KV M-8110-UL-95KV M-8110-HP-110KV
Propeller 28*9.2"/29*9.5"/30*9.8" 28*9.2"/29*9.5"/30*9.8" 28*9.2"/29*9.5"/30*9.8" 28*9.2"/29*9.5"
30*9.8"/32*10.5"		 28*9.2"/29*9.5"
30*9.8"/32*10.5"
ESC XRotor Pro-H60A-14S XRotor Pro-H60A-14S XRotor Pro-H60A-14S XRotor Pro-H60A-14S XRotor Pro-H60A-14S
Battery 12S LiPo 12S LiPo 6S LiPo 12S LiPo 12S LiPo
Thrust/rotor 2.5~3.5kg 2.5~3.5kg 2.5~3.5kg 3.0~4.0kg 3.0~4.0kg
Takeoff weight of quadrotor 10~14kg 10~14kg 10~14kg 12.0~16.0kg 12.0~16.0kg
M 8108 85KV+GP29*9.5" Load performance parameters
M 8108 85KV+GP29*9.5"Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

TTemperature(℃)

46V (12S LiPo)

GP29*9.5"

33%

1171

1.5

69.6

1270

16.8

0.41

66.1°C

35%

1285

1.7

78.6

1331

16.3

0.45

37%

1413

1.9

89.4

1398

15.8

0.49

39%

1552

2.2

101.9

1467

15.2

0.54

42%

1778

2.7

123.7

1575

14.4

0.62

45%

2021

3.2

148.8

1683

13.6

0.70

48%

2279

3.8

176.9

1789

12.9

0.79

51%

2549

4.5

207.6

1891

12.3

0.88

54%

2828

5.2

240.8

1989

11.7

0.97

57%

3117

6.0

276.4

2083

11.3

1.06

60%

3412

6.8

314.6

2172

10.8

1.16

63%

3715

7.7

355.5

2259

10.5

1.26

66%

4024

8.7

399.5

2344

10.1

1.36

69%

4339

9.7

446.8

2428

9.7

1.47

72%

4657

10.8

497.7

2512

9.4

1.58

75%

4977

12.0

552.1

2596

9.0

1.69

78%

5296

13.2

609.5

2680

8.7

1.80

81%

5611

14.5

669.0

2763

8.4

1.91

84%

5917

15.8

729.0

2843

8.1

2.01

87%

6208

17.1

787.3

2916

7.9

2.11

90%

6476

18.3

841.4

2979

7.7

2.20

100%

7060

20.7

954.7

3092

7.4

2.37
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.
M 8108 100KV+GP28*9.2" Load performance parameters
M 8108 100KV+GP28*9.2" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

TTemperature(℃)

46V (12S LiPo)

GP28*9.2"

33%

1438

2.1

97.8

1508

14.7

0.46

73.2°C

35%

1599

2.4

111.7

1587

14.3

0.52

37%

1778

2.8

128.5

1672

13.8

0.57

39%

1972

3.2

147.9

1760

13.3

0.64

42%

2281

3.9

181.4

1894

12.6

0.74

45%

2605

4.8

219.3

2024

11.9

0.84

48%

2937

5.7

260.7

2149

11.3

0.95

51%

3273

6.6

305.0

2268

10.7

1.05

54%

3613

7.6

351.9

2381

10.3

1.16

57%

3955

8.7

401.4

2488

9.9

1.27

60%

4301

9.9

454.0

2592

9.5

1.38

63%

4654

11.1

510.2

2692

9.1

1.49

66%

5014

12.4

570.7

2791

8.8

1.60

69%

5383

13.8

636.1

2890

8.5

1.72

72%

5763

15.4

707.4

2988

8.1

1.84

75%

6151

17.1

784.7

3087

7.8

1.97

78%

6547

18.9

868.1

3185

7.5

2.10

81%

6946

20.8

956.6

3282

7.3

2.24

84%

7338

22.8

1048.2

3373

7.0

2.37

87%

7714

24.8

1139.2

3458

6.8

2.50

90%

8059

26.6

1224.7

3530

6.6

2.61

100%

8693

30.1

1384.4

3647

6.3

2.81
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.
M 8108 150KV+GP28*9.2" Load performance parameters
M 8108 150KV+GP28*9.2"Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

TTemperature(℃)

46V (12S LiPo)

GP28*9.2"

33%

871

2.0

47.2

1096

18.5

0.30

54.2°C

35%

968

2.3

53.7

1151

18.0

0.33

37%

1070

2.7

61.2

1207

17.5

0.37

39%

1178

3.0

69.5

1266

16.9

0.40

42%

1349

3.6

83.6

1355

16.1

0.46

45%

1529

4.3

99.6

1445

15.4

0.52

48%

1720

5.1

117.4

1535

14.6

0.59

51%

1919

5.9

137.0

1623

14.0

0.66

54%

2127

6.9

158.4

1709

13.4

0.72

57%

2344

7.9

181.6

1793

12.9

0.80

60%

2569

9.0

206.7

1875

12.4

0.87

63%

2802

10.1

234.0

1954

12.0

0.95

66%

3043

11.4

263.5

2032

11.5

1.03

69%

3290

12.8

295.3

2109

11.1

1.11

72%

3542

14.3

329.6

2185

10.7

1.19

75%

3798

366.3

676.5

2262

10.4

1.28

78%

4054

17.6

404.9

2339

10.0

1.37

81%

4307

19.3

445.0

2414

9.7

1.46

84%

4554

21.0

485.3

2487

9.4

1.54

87%

4789

22.8

524.7

2554

9.1

1.62

90%

5005

24.3

561.3

2611

8.9

1.70

100%

5483

27.8

640.0

2712

8.6

1.84
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.
M 8110 95KV+GP29*9.5" Load performance parameters
M 8110 95KV+GP29*9.5"Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

TTemperature(℃)

46V (12S LiPo)

GP29*9.5"

33%

1241

1.9

88.0

1367

14.1

0.43

65.1°C

35%

1351

2.1

98.1

1428

13.8

0.47

37%

1491

2.4

110.8

1501

13.5

0.52

39%

1653

2.7

125.7

1581

13.2

0.57

42%

1929

3.3

151.8

1707

12.7

0.67

45%

2232

3.9

181.8

1833

12.3

0.77

48%

2551

4.7

215.7

1955

11.8

0.87

51%

2877

5.5

253.3

2071

11.4

0.98

54%

3207

6.4

294.4

2182

10.9

1.09

57%

3539

7.4

338.7

2289

10.4

1.21

60%

3870

8.4

386.3

2392

10.0

1.32

63%

4203

9.5

437.1

2492

9.6

1.44

66%

4541

10.7

491.1

2591

9.2

1.55

69%

4886

11.9

548.8

2689

8.9

1.67

72%

5242

13.3

610.5

2787

8.6

1.80

75%

5615

14.7

676.5

2885

8.3

1.93

78%

6007

16.2

747.3

2983

8.0

2.06

81%

6422

17.9

823.1

3079

7.8

2.20

84%

6862

19.6

903.9

3173

7.6

2.34

87%

7330

21.5

990.1

3261

7.4

2.49

90%

7823

23.5

1082.3

3345

7.2

2.64

100%

9515

31.3

1439.5

3616

6.6

3.20
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.
M 8110 110KV+GP28*9.2"Load performance parameters
M 8110 110KV+GP28*9.2"Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

TTemperature(℃)

46V (12S LiPo)

GP28*9.2"

33%

1284

2.2

99.4

1484

12.9

0.44

68.5°C

35%

1404

2.4

109.1

1550

12.9

0.47

37%

1553

2.6

121.8

1629

12.7

0.52

39%

1725

3.0

137.6

1717

12.5

0.58

42%

2015

3.6

166.5

1855

12.1

0.67

45%

2332

4.4

201.2

1996

11.6

0.77

48%

2665

5.2

240.6

2134

11.1

0.88

51%

3007

6.2

283.8

2266

10.6

0.99

54%

3353

7.2

330.1

2391

10.2

1.10

57%

3699

8.2

379.0

2509

9.8

1.22

60%

4045

9.3

430.1

2622

9.4

1.33

63%

4392

10.5

483.5

2729

9.1

1.44

66%

4740

11.7

539.5

2834

8.8

1.55

69%

5094

13.0

598.7

2936

8.5

1.67

72%

5457

14.4

661.8

3038

8.2

1.78

75%

5833

15.8

729.9

3140

8.0

1.91

78%

6228

17.5

804.2

3244

7.7

2.03

81%

6645

19.2

885.7

3350

7.5

2.17

84%

7090

21.2

975.7

3457

7.3

2.32

87%

7565

23.3

1075.0

3566

7.0

2.47

90%

8074

25.7

1183.8

3674

6.8

2.64

100%

9915

34.0

1565.5

3964

6.3

3.19
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.
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M 8108 UL Specification
M 8110 UL Specification
M 8108 UL Load performance parameters
M 8110 UL Load performance parameters
M 8108 UL 3D Model Drawing
M 8110 UL 3D Model Drawing
M 8108 UL CAD
M 8110 UL CAD

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M 8108/8110 UL
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M 8108 / 8110
Industrial Mu ltirotor Drone Motors
LOAD PERFORMANCE PARAMETERS:
High efficiency increases
battery lifespan
  • The recommended
    pulling force is
    3kg+
  • The force efficiency is
    11g/w+
  • Increases battery
    lifespan
The recommended pulling force is
3kg
Takeoff weight of quadrotor
12kg
The force efficiency is
11g/w
  • (12S 36Ah)
  • The whole machine
    10kg
  • The endurance
    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 CNCmachined rotor bracket High-strength aviation aluminum7075-T651
  • 16AWGhighly flexible silicone wire, low resistivity and good toughness
  • High-performance iron core punched from0.2mm low-loss silicon steel sheet
M 8108 UL CAD
M 8110 UL CAD
Model
M 8108 85KV UL M 8108 100KV UL M 8108 150KV UL M 8110 95KV UL M 8110 110KV UL
Specification
Motor Size Φ87.1*H25.4mm Φ87.1*H25.4mm Φ87.1*H25.4mm Φ87.1*H27.4mm Φ87.1*H27.4mm
Stator Size Φ81mm Φ81mm 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 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℃ 200℃ 200℃
Magnet 180℃ 180℃ 180℃ 180℃ 180℃
Isolation test 500V AC high voltage resistance test 500V AC high voltage resistance test 500V AC high voltage resistance test 500V AC high voltage resistance test 500V AC high voltage resistance test
Protection level IPX5 IPX5 IPX5 IPX5 IPX5
Slot& Pole 36N 42P 36N 42P 36N 42P 36N 42P 36N 42P
Dynamic balance ≤10mg ≤10mg ≤10mg ≤10mg ≤10mg
Bearing Water proof bearing Water proof 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 4×M3@D20mm+4×M4@D23mm 4×M3@D20mm+4×M4@D23mm
Motor mounting dimensions 4×M4@D36mm 4×M4@D36mm 4×M4@D36mm 4×M4@D36mm 4×M4@D36mm
KV 85 100 150 95 110
Battery(LiPo) 12S LiPo 12S LiPo 6S LiPo 12S LiPo 12S LiPo
No-load current 0.91A 1.19A 1.41A 1.1A 1.27A
Maximum current (Non-hermetic Ambient Temperature ≤ 25℃） 20.8A 33.8A 27.8A 43.3A 39.2A
Max power 950W 1550W 640W 2000W 1800W
Max thrust 7.2kg 9.2kg 5.5kg 11.4kg 11.1kg
Resistance 239.5 mΩ 165.2 mΩ 82.8 mΩ 132.9 mΩ 112.3 mΩ
Wire Size 16 AWG 16 AWG 16 AWG 16 AWG 16 AWG
Wire length 100 mm 100 mm 100 mm 100 mm 100 mm
Weight（With wire） 237.4g 238.3g 242.8g 300.5g 301.5g
Recommended application combinations
Motor M-8108-UL-85KV M-8108-UL-100KV M-8108-UL-150KV M-8110-UL-95KV M-8110-HP-110KV
Propeller 28*9.2"/29*9.5"/30*9.8" 28*9.2"/29*9.5"/30*9.8" 28*9.2"/29*9.5"/30*9.8" 28*9.2"/29*9.5"
30*9.8"/32*10.5"		 28*9.2"/29*9.5"
30*9.8"/32*10.5"
ESC XRotor Pro-H60A-14S XRotor Pro-H60A-14S XRotor Pro-H60A-14S XRotor Pro-H60A-14S XRotor Pro-H60A-14S
Battery 12S LiPo 12S LiPo 6S LiPo 12S LiPo 12S LiPo
Thrust/rotor 2.5~3.5kg 2.5~3.5kg 2.5~3.5kg 3.0~4.0kg 3.0~4.0kg
Takeoff weight of quadrotor 10~14kg 10~14kg 10~14kg 12.0~16.0kg 12.0~16.0kg
M 8108 85KV+GP29*9.5" Load performance parameters
M 8108 85KV+GP29*9.5"Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

TTemperature(℃)

46V (12S LiPo)

GP29*9.5"

33%

1171

1.5

69.6

1270

16.8

0.41

66.1°C

35%

1285

1.7

78.6

1331

16.3

0.45

37%

1413

1.9

89.4

1398

15.8

0.49

39%

1552

2.2

101.9

1467

15.2

0.54

42%

1778

2.7

123.7

1575

14.4

0.62

45%

2021

3.2

148.8

1683

13.6

0.70

48%

2279

3.8

176.9

1789

12.9

0.79

51%

2549

4.5

207.6

1891

12.3

0.88

54%

2828

5.2

240.8

1989

11.7

0.97

57%

3117

6.0

276.4

2083

11.3

1.06

60%

3412

6.8

314.6

2172

10.8

1.16

63%

3715

7.7

355.5

2259

10.5

1.26

66%

4024

8.7

399.5

2344

10.1

1.36

69%

4339

9.7

446.8

2428

9.7

1.47

72%

4657

10.8

497.7

2512

9.4

1.58

75%

4977

12.0

552.1

2596

9.0

1.69

78%

5296

13.2

609.5

2680

8.7

1.80

81%

5611

14.5

669.0

2763

8.4

1.91

84%

5917

15.8

729.0

2843

8.1

2.01

87%

6208

17.1

787.3

2916

7.9

2.11

90%

6476

18.3

841.4

2979

7.7

2.20

100%

7060

20.7

954.7

3092

7.4

2.37
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.
M 8108 100KV+GP28*9.2" Load performance parameters
M 8108 100KV+GP28*9.2" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

TTemperature(℃)

46V (12S LiPo)

GP28*9.2"

33%

1438

2.1

97.8

1508

14.7

0.46

73.2°C

35%

1599

2.4

111.7

1587

14.3

0.52

37%

1778

2.8

128.5

1672

13.8

0.57

39%

1972

3.2

147.9

1760

13.3

0.64

42%

2281

3.9

181.4

1894

12.6

0.74

45%

2605

4.8

219.3

2024

11.9

0.84

48%

2937

5.7

260.7

2149

11.3

0.95

51%

3273

6.6

305.0

2268

10.7

1.05

54%

3613

7.6

351.9

2381

10.3

1.16

57%

3955

8.7

401.4

2488

9.9

1.27

60%

4301

9.9

454.0

2592

9.5

1.38

63%

4654

11.1

510.2

2692

9.1

1.49

66%

5014

12.4

570.7

2791

8.8

1.60

69%

5383

13.8

636.1

2890

8.5

1.72

72%

5763

15.4

707.4

2988

8.1

1.84

75%

6151

17.1

784.7

3087

7.8

1.97

78%

6547

18.9

868.1

3185

7.5

2.10

81%

6946

20.8

956.6

3282

7.3

2.24

84%

7338

22.8

1048.2

3373

7.0

2.37

87%

7714

24.8

1139.2

3458

6.8

2.50

90%

8059

26.6

1224.7

3530

6.6

2.61

100%

8693

30.1

1384.4

3647

6.3

2.81
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.
M 8108 150KV+GP28*9.2" Load performance parameters
M 8108 150KV+GP28*9.2"Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

TTemperature(℃)

46V (12S LiPo)

GP28*9.2"

33%

871

2.0

47.2

1096

18.5

0.30

54.2°C

35%

968

2.3

53.7

1151

18.0

0.33

37%

1070

2.7

61.2

1207

17.5

0.37

39%

1178

3.0

69.5

1266

16.9

0.40

42%

1349

3.6

83.6

1355

16.1

0.46

45%

1529

4.3

99.6

1445

15.4

0.52

48%

1720

5.1

117.4

1535

14.6

0.59

51%

1919

5.9

137.0

1623

14.0

0.66

54%

2127

6.9

158.4

1709

13.4

0.72

57%

2344

7.9

181.6

1793

12.9

0.80

60%

2569

9.0

206.7

1875

12.4

0.87

63%

2802

10.1

234.0

1954

12.0

0.95

66%

3043

11.4

263.5

2032

11.5

1.03

69%

3290

12.8

295.3

2109

11.1

1.11

72%

3542

14.3

329.6

2185

10.7

1.19

75%

3798

366.3

676.5

2262

10.4

1.28

78%

4054

17.6

404.9

2339

10.0

1.37

81%

4307

19.3

445.0

2414

9.7

1.46

84%

4554

21.0

485.3

2487

9.4

1.54

87%

4789

22.8

524.7

2554

9.1

1.62

90%

5005

24.3

561.3

2611

8.9

1.70

100%

5483

27.8

640.0

2712

8.6

1.84
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.
M 8110 95KV+GP29*9.5" Load performance parameters
M 8110 95KV+GP29*9.5"Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

TTemperature(℃)

46V (12S LiPo)

GP29*9.5"

33%

1241

1.9

88.0

1367

14.1

0.43

65.1°C

35%

1351

2.1

98.1

1428

13.8

0.47

37%

1491

2.4

110.8

1501

13.5

0.52

39%

1653

2.7

125.7

1581

13.2

0.57

42%

1929

3.3

151.8

1707

12.7

0.67

45%

2232

3.9

181.8

1833

12.3

0.77

48%

2551

4.7

215.7

1955

11.8

0.87

51%

2877

5.5

253.3

2071

11.4

0.98

54%

3207

6.4

294.4

2182

10.9

1.09

57%

3539

7.4

338.7

2289

10.4

1.21

60%

3870

8.4

386.3

2392

10.0

1.32

63%

4203

9.5

437.1

2492

9.6

1.44

66%

4541

10.7

491.1

2591

9.2

1.55

69%

4886

11.9

548.8

2689

8.9

1.67

72%

5242

13.3

610.5

2787

8.6

1.80

75%

5615

14.7

676.5

2885

8.3

1.93

78%

6007

16.2

747.3

2983

8.0

2.06

81%

6422

17.9

823.1

3079

7.8

2.20

84%

6862

19.6

903.9

3173

7.6

2.34

87%

7330

21.5

990.1

3261

7.4

2.49

90%

7823

23.5

1082.3

3345

7.2

2.64

100%

9515

31.3

1439.5

3616

6.6

3.20
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.
M 8110 110KV+GP28*9.2"Load performance parameters
M 8110 110KV+GP28*9.2"Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

TTemperature(℃)

46V (12S LiPo)

GP28*9.2"

33%

1284

2.2

99.4

1484

12.9

0.44

68.5°C

35%

1404

2.4

109.1

1550

12.9

0.47

37%

1553

2.6

121.8

1629

12.7

0.52

39%

1725

3.0

137.6

1717

12.5

0.58

42%

2015

3.6

166.5

1855

12.1

0.67

45%

2332

4.4

201.2

1996

11.6

0.77

48%

2665

5.2

240.6

2134

11.1

0.88

51%

3007

6.2

283.8

2266

10.6

0.99

54%

3353

7.2

330.1

2391

10.2

1.10

57%

3699

8.2

379.0

2509

9.8

1.22

60%

4045

9.3

430.1

2622

9.4

1.33

63%

4392

10.5

483.5

2729

9.1

1.44

66%

4740

11.7

539.5

2834

8.8

1.55

69%

5094

13.0

598.7

2936

8.5

1.67

72%

5457

14.4

661.8

3038

8.2

1.78

75%

5833

15.8

729.9

3140

8.0

1.91

78%

6228

17.5

804.2

3244

7.7

2.03

81%

6645

19.2

885.7

3350

7.5

2.17

84%

7090

21.2

975.7

3457

7.3

2.32

87%

7565

23.3

1075.0

3566

7.0

2.47

90%

8074

25.7

1183.8

3674

6.8

2.64

100%

9915

34.0

1565.5

3964

6.3

3.19
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.
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M 8108 UL Specification
M 8110 UL Specification
M 8108 UL Load performance parameters
M 8110 UL Load performance parameters
M 8108 UL 3D Model Drawing
M 8110 UL 3D Model Drawing
M 8108 UL CAD
M 8110 UL CAD

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