M 8108/8110 HP
HM 8108 / 8110
Industrial Multirotor Drone Motors
Load Performance Parameters:
HM8108 HM8110
High Efficiency, Long Endurance
  • The recommended thrust is
    3kg+
  • The efficiency is
    11g/w+
  • Long flight time
The recommended
thrust is
3kg
The maximum takeoff weight is
12kg
The efficiency is
11g/w
  • (12S 36Ah)
  • 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,
    optimized fan ports effectively
    improve the protection level.
  • 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
  • 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 ability.
  • 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 premium 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-T651
  • precisionCNC
    machined rotor bracket
  • The outer rotor casing is made of
    20# seamless steel rotor with nickel
    electrophoresis design, which has excellent magnetic conductivity
    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 Application
Combinations
  • Motor
    M 8108 HP
    Battery
    12S 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
    M 8110 HP
    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 HP CAD
Model
M 8108 85KV HP M 8108 100KV HP M 8110 95KV HP M 8110 110KV HP
Specification
Motor Size Φ87.1*H26.9mm Φ87.1*H26.9mm Φ87.1*H28.9mm Φ87.1*H28.9mm
Stator Size Φ81.0mm Φ81.0mm Φ81.0mm Φ81.0mm
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
Enamelled wire 220℃ 220℃ 220℃ 220℃
Magnet 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
Protection level IP45 IP45 IP45 IP45
Slot& Pole 36N 42P 36N 42P 36N 42P 36N 42P
Dynamic balance ≤10mg ≤10mg ≤10mg ≤10mg
Bearing Water proof bearing Water proof bearing Water proof bearing Water proof bearing
Motor axle diameter shaft sleeve Φ10mm shaft sleeve Φ10mm shaft sleeve Φ10mm shaft sleeve Φ10mm
Props mounting dimensions 4×M4@D23+4×M3@D20 4×M4@D23+4×M3@D20 4×M4@D23+4×M3@D20 4×M4@D23+4×M3@D20
Motor mounting dimensions 4×M4@D36 4×M4@D36 4×M4@D36 4×M4@D36
KV 85 100 95 110
Battery(LiPo) 12S LiPo 12S LiPo 12S LiPo 12S LiPo
No-load current 0.67 A 1.11A 1.1 A 1.27A
Maximum current
(Non-hermetic Ambient Temperature ≤ 25℃）		 27.2 A 34.3A 43.2A 39.2A
Max power 950W 1572W 1992W 1803W
Max thrust 7.2kg 9.3kg 11.3kg 11kg
Resistance 241.2 mΩ 163.3 mΩ 132.9 mΩ 112.3 mΩ
Wire Size 16 AWG 16 AWG 16 AWG 16 AWG
Wire length 100 mm 100 mm 100 mm 100 mm
Weight（With wire） 270g 271g 315g 317g
Recommended application combinations
Motor M-8108-HP-85KV M-8108-HP-100KV M-8110-HP-95KV M-8110-HP-110KV
Propeller GP28×9.2"/GP29×9.5"/ML30*9.8" GP28×9.2"/GP29×9.5"/ML30*9.8" GP29×9.5"/ML30*9.8"/GP32×10.5" GP29×9.5"/ML30*9.8"/GP32×10.5"
ESC XRotor Pro-H60A-14S XRotor Pro-H60A-14S XRotor Pro-H60A-14S XRotor Pro-H60A-14S
Battery 12S LiPo 12S LiPo 12S LiPo 12S LiPo
Thrust/rotor (kg) 2.5~3.5kg 2.5~3.5kg 3.0~4.0kg 3.0~4.0kg
Takeoff weight of quadrotor(kg) 10.0~14.0kg 10.0~14.0kg 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)

Temperature(℃)

46V (12S LiPo)

GP29*9.5"

33%

951

1.4

63.0

1191

15.1

0.34

62.0°C

35%

1033

1.5

70.2

1243

14.7

0.37

37%

1136

1.7

79.1

1305

14.4

0.40

39%

1254

1.9

89.4

1372

14.0

0.44

42%

1455

2.3

107.0

1478

13.6

0.51

45%

1676

2.8

127.1

1585

13.2

0.59

48%

1909

3.2

149.3

1690

12.8

0.66

51%

2150

3.8

173.6

1791

12.4

0.74

54%

2396

4.3

200.1

1887

12.0

0.83

57%

2644

5.0

228.6

1981

11.6

0.91

60%

2895

5.6

259.4

2071

11.2

0.99

63%

3148

6.3

292.4

2160

10.8

1.08

66%

3405

7.1

327.7

2247

10.4

1.17

69%

3669

7.9

365.7

2333

10.0

1.26

72%

3941

8.8

406.4

2419

9.7

1.35

75%

4223

9.8

450.3

2504

9.4

1.45

78%

4519

10.8

497.4

2589

9.1

1.55

81%

4830

11.9

548.0

2671

8.8

1.65

84%

5157

13.1

602.2

2752

8.6

1.76

87%

5501

14.3

660.0

2828

8.3

1.87

90%

5862

15.7

721.4

2900

8.1

1.98

100%

7085

20.5

945.5

3134

7.5

2.36
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)

Temperature(℃)

46V (12S LiPo)

GP28*9.2"

33%

1133

1.7

80.0

1398

14.2

0.38

70°C

35%

1232

1.9

89.1

1457

13.8

0.41

37%

1367

2.2

101.4

1532

13.5

0.46

39%

1527

2.5

116.2

1617

13.1

0.51

42%

1799

3.1

142.4

1753

12.6

0.60

45%

2093

3.7

172.4

1888

12.1

0.69

48%

2394

4.5

205.8

2019

11.6

0.79

51%

2695

5.3

241.9

2141

11.1

0.89

54%

2990

6.1

280.4

2257

10.7

0.98

57%

3280

7.0

320.9

2365

10.2

1.08

60%

3565

7.9

363.4

2469

9.8

1.17

63%

3852

8.9

408.5

2570

9.4

1.27

66%

4145

9.9

456.7

2669

9.1

1.36

69%

4450

11.1

509.0

2769

8.7

1.46

72%

4776

12.3

566.4

2869

8.4

1.57

75%

5126

13.7

629.6

2971

8.1

1.68

78%

5506

15.2

699.1

3073

7.9

1.8

81%

5917

16.8

774.9

3173

7.6

1.94

84%

6357

18.6

856.9

3268

7.4

2.08

87%

6822

20.5

944.7

3356

7.2

2.22

90%

7302

22.5

1038.5

3438

7.0

2.37

100%

8711

29.9

1375.9

3721

6.3

2.83
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+ML30*9.8" Load performance parameters
M 8110 95KV+ML30*9.8"Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature(℃)

46V (12S LiPo)

ML30*9.8"

33%

1281

1.9

89.6

1366

14.3

0.45

68.0°C

35%

1421

2.2

101.3

1433

14.0

0.49

37%

1575

2.5

114.8

1505

13.7

0.54

39%

1743

2.8

130.1

1580

13.4

0.60

42%

2015

3.4

156.5

1698

12.9

0.69

45%

2311

4.1

186.9

1818

12.4

0.79

48%

2626

4.8

221.2

1939

11.9

0.89

51%

2956

5.6

259.3

2057

11.4

1.00

54%

3298

6.5

301.1

2172

11.0

1.12

57%

3650

7.5

346.4

2282

10.5

1.23

60%

4008

8.6

395.1

2388

10.1

1.35

63%

4371

9.7

447.0

2490

9.8

1.47

66%

4736

10.9

502.2

2588

9.4

1.59

69%

5105

12.2

560.7

2683

9.1

1.71

72%

5477

13.5

622.6

2776

8.8

1.84

75%

5853

14.9

688.3

2870

8.5

1.96

78%

6237

16.5

758.3

2963

8.2

2.09

81%

6631

18.1

833.2

3059

8.0

2.23

84%

7040

19.8

913.9

3157

7.7

2.37

87%

7472

21.8

1001.6

3259

7.5

2.52

90%

7933

23.8

1097.4

3363

7.2

2.68

100%

9708

31.6

1454.1

3628

6.7

3.22
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+GP29*9.5" Load performance parameters
M 8110 110KV+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)

Temperature(℃)

46V (12S LiPo)

GP29*9.5"

33%

1420

2.4

108.5

1461

13.1

0.50

76.0°C

35%

1581

2.6

120.5

1533

13.1

0.55

37%

1761

2.9

135.5

1612

13.0

0.61

39%

1957

3.3

153.5

1696

12.7

0.68

42%

2276

4.0

186.1

1827

12.2

0.78

45%

2619

4.9

224.8

1960

11.7

0.90

48%

2980

5.8

268.9

2092

11.1

1.02

51%

3353

6.9

317.7

2220

10.6

1.15

54%

3735

8.0

370.3

2342

10.1

1.27

57%

4122

9.3

426.3

2458

9.7

1.40

60%

4511

10.5

485.2

2567

9.3

1.53

63%

4902

11.9

547.2

2672

9.0

1.66

66%

5294

13.3

612.2

2772

8.6

1.79

69%

5687

14.8

680.8

2869

8.4

1.93

72%

6084

16.4

753.4

2965

8.1

2.06

75%

6487

18.0

831.0

3061

7.8

2.20

78%

6898

19.9

914.5

3159

7.5

2.34

81%

7323

21.8

1005.3

3260

7.3

2.49

84%

7767

24.0

1104.7

3364

7.0

2.64

87%

8235

26.4

1214.2

3474

6.8

2.81

90%

8735

29.0

1334.9

3586

6.5

2.99

100%

10624

38.5

1772.7

3870

6.0

3.60
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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HM 8108 HP Specification
HM 8110 HP Specification
HM 8108 HP Load performance parameters
HM 8110 HP Load performance parameters
HM 8108 HP CAD
HM 8108 HP 3D Model Drawing
HM 8110 HP 3D Model Drawing

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M 8108/8110 HP
Overview Specifications Support Accessories Detail Contact us Shop
M 8108 / 8110
Industrial Multirotor 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 IP45.
  • 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 HP CAD
Model
M 8108 85KV HP M 8108 100KV HP M 8110 95KV HP M 8110 110KV HP
Specification
Motor Size Φ87.1*H26.9mm Φ87.1*H26.9mm Φ87.1*H28.9mm Φ87.1*H28.9mm
Stator Size Φ81.0mm Φ81.0mm Φ81.0mm Φ81.0mm
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
Enamelled wire 220℃ 220℃ 220℃ 220℃
Magnet 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
Protection level IP45 IP45 IP45 IP45
Slot& Pole 36N 42P 36N 42P 36N 42P 36N 42P
Dynamic balance ≤10mg ≤10mg ≤10mg ≤10mg
Bearing Water proof bearing Water proof bearing Water proof bearing Water proof bearing
Motor axle diameter shaft sleeve Φ10mm shaft sleeve Φ10mm shaft sleeve Φ10mm shaft sleeve Φ10mm
Props mounting dimensions 4×M4@D23+4×M3@D20 4×M4@D23+4×M3@D20 4×M4@D23+4×M3@D20 4×M4@D23+4×M3@D20
Motor mounting dimensions 4×M4@D36 4×M4@D36 4×M4@D36 4×M4@D36
KV 85 100 95 110
Battery(LiPo) 12S LiPo 12S LiPo 12S LiPo 12S LiPo
No-load current 0.67 A 1.11A 1.1 A 1.27A
Maximum current
(Non-hermetic Ambient Temperature ≤ 25℃）		 27.2 A 34.3A 43.2A 39.2A
Max power 950W 1572W 1992W 1803W
Max thrust 7.2kg 9.3kg 11.3kg 11kg
Resistance 241.2 mΩ 163.3 mΩ 132.9 mΩ 112.3 mΩ
Wire Size 16 AWG 16 AWG 16 AWG 16 AWG
Wire length 100 mm 100 mm 100 mm 100 mm
Weight（With wire） 270g 271g 315g 317g
Recommended application combinations
Motor M-8108-HP-85KV M-8108-HP-100KV M-8110-HP-95KV M-8110-HP-110KV
Propeller GP28×9.2"/GP29×9.5"/ML30*9.8" GP28×9.2"/GP29×9.5"/ML30*9.8" GP29×9.5"/ML30*9.8"/GP32×10.5" GP29×9.5"/ML30*9.8"/GP32×10.5"
ESC XRotor Pro-H60A-14S XRotor Pro-H60A-14S XRotor Pro-H60A-14S XRotor Pro-H60A-14S
Battery 12S LiPo 12S LiPo 12S LiPo 12S LiPo
Thrust/rotor (kg) 2.5~3.5kg 2.5~3.5kg 3.0~4.0kg 3.0~4.0kg
Takeoff weight of quadrotor(kg) 10.0~14.0kg 10.0~14.0kg 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)

Temperature(℃)

46V (12S LiPo)

GP29*9.5"

33%

951

1.4

63.0

1191

15.1

0.34

62.0°C

35%

1033

1.5

70.2

1243

14.7

0.37

37%

1136

1.7

79.1

1305

14.4

0.40

39%

1254

1.9

89.4

1372

14.0

0.44

42%

1455

2.3

107.0

1478

13.6

0.51

45%

1676

2.8

127.1

1585

13.2

0.59

48%

1909

3.2

149.3

1690

12.8

0.66

51%

2150

3.8

173.6

1791

12.4

0.74

54%

2396

4.3

200.1

1887

12.0

0.83

57%

2644

5.0

228.6

1981

11.6

0.91

60%

2895

5.6

259.4

2071

11.2

0.99

63%

3148

6.3

292.4

2160

10.8

1.08

66%

3405

7.1

327.7

2247

10.4

1.17

69%

3669

7.9

365.7

2333

10.0

1.26

72%

3941

8.8

406.4

2419

9.7

1.35

75%

4223

9.8

450.3

2504

9.4

1.45

78%

4519

10.8

497.4

2589

9.1

1.55

81%

4830

11.9

548.0

2671

8.8

1.65

84%

5157

13.1

602.2

2752

8.6

1.76

87%

5501

14.3

660.0

2828

8.3

1.87

90%

5862

15.7

721.4

2900

8.1

1.98

100%

7085

20.5

945.5

3134

7.5

2.36
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)

Temperature(℃)

46V (12S LiPo)

GP28*9.2"

33%

1133

1.7

80.0

1398

14.2

0.38

70°C

35%

1232

1.9

89.1

1457

13.8

0.41

37%

1367

2.2

101.4

1532

13.5

0.46

39%

1527

2.5

116.2

1617

13.1

0.51

42%

1799

3.1

142.4

1753

12.6

0.60

45%

2093

3.7

172.4

1888

12.1

0.69

48%

2394

4.5

205.8

2019

11.6

0.79

51%

2695

5.3

241.9

2141

11.1

0.89

54%

2990

6.1

280.4

2257

10.7

0.98

57%

3280

7.0

320.9

2365

10.2

1.08

60%

3565

7.9

363.4

2469

9.8

1.17

63%

3852

8.9

408.5

2570

9.4

1.27

66%

4145

9.9

456.7

2669

9.1

1.36

69%

4450

11.1

509.0

2769

8.7

1.46

72%

4776

12.3

566.4

2869

8.4

1.57

75%

5126

13.7

629.6

2971

8.1

1.68

78%

5506

15.2

699.1

3073

7.9

1.8

81%

5917

16.8

774.9

3173

7.6

1.94

84%

6357

18.6

856.9

3268

7.4

2.08

87%

6822

20.5

944.7

3356

7.2

2.22

90%

7302

22.5

1038.5

3438

7.0

2.37

100%

8711

29.9

1375.9

3721

6.3

2.83
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+ML30*9.8" Load performance parameters
M 8110 95KV+ML30*9.8"Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature(℃)

46V (12S LiPo)

ML30*9.8"

33%

1281

1.9

89.6

1366

14.3

0.45

68.0°C

35%

1421

2.2

101.3

1433

14.0

0.49

37%

1575

2.5

114.8

1505

13.7

0.54

39%

1743

2.8

130.1

1580

13.4

0.60

42%

2015

3.4

156.5

1698

12.9

0.69

45%

2311

4.1

186.9

1818

12.4

0.79

48%

2626

4.8

221.2

1939

11.9

0.89

51%

2956

5.6

259.3

2057

11.4

1.00

54%

3298

6.5

301.1

2172

11.0

1.12

57%

3650

7.5

346.4

2282

10.5

1.23

60%

4008

8.6

395.1

2388

10.1

1.35

63%

4371

9.7

447.0

2490

9.8

1.47

66%

4736

10.9

502.2

2588

9.4

1.59

69%

5105

12.2

560.7

2683

9.1

1.71

72%

5477

13.5

622.6

2776

8.8

1.84

75%

5853

14.9

688.3

2870

8.5

1.96

78%

6237

16.5

758.3

2963

8.2

2.09

81%

6631

18.1

833.2

3059

8.0

2.23

84%

7040

19.8

913.9

3157

7.7

2.37

87%

7472

21.8

1001.6

3259

7.5

2.52

90%

7933

23.8

1097.4

3363

7.2

2.68

100%

9708

31.6

1454.1

3628

6.7

3.22
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+GP29*9.5" Load performance parameters
M 8110 110KV+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)

Temperature(℃)

46V (12S LiPo)

GP29*9.5"

33%

1420

2.4

108.5

1461

13.1

0.50

76.0°C

35%

1581

2.6

120.5

1533

13.1

0.55

37%

1761

2.9

135.5

1612

13.0

0.61

39%

1957

3.3

153.5

1696

12.7

0.68

42%

2276

4.0

186.1

1827

12.2

0.78

45%

2619

4.9

224.8

1960

11.7

0.90

48%

2980

5.8

268.9

2092

11.1

1.02

51%

3353

6.9

317.7

2220

10.6

1.15

54%

3735

8.0

370.3

2342

10.1

1.27

57%

4122

9.3

426.3

2458

9.7

1.40

60%

4511

10.5

485.2

2567

9.3

1.53

63%

4902

11.9

547.2

2672

9.0

1.66

66%

5294

13.3

612.2

2772

8.6

1.79

69%

5687

14.8

680.8

2869

8.4

1.93

72%

6084

16.4

753.4

2965

8.1

2.06

75%

6487

18.0

831.0

3061

7.8

2.20

78%

6898

19.9

914.5

3159

7.5

2.34

81%

7323

21.8

1005.3

3260

7.3

2.49

84%

7767

24.0

1104.7

3364

7.0

2.64

87%

8235

26.4

1214.2

3474

6.8

2.81

90%

8735

29.0

1334.9

3586

6.5

2.99

100%

10624

38.5

1772.7

3870

6.0

3.60
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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HM 8108 HP Specification
HM 8110 HP Specification
HM 8108 HP Load performance parameters
HM 8110 HP Load performance parameters
HM 8108 HP CAD
HM 8108 HP 3D Model Drawing
HM 8110 HP 3D Model Drawing

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