M 6208 UL
6208-155KV/310KV
Industrial-level Multi-rotor UAV Motor
Reliable and Efficient,
Ideal for Long Endurance.
Designed for high-end industrial-grade multi-rotor drone applications. It is widely used in aerial
photography, surveying, monitoring, inspection, public safety and other scenarios.
The Sharp and Distinct Edges
Stands Out Remarkably
The rotor is well balanced, featuring
an ultimate hollow design for maximum
weight reduction. The motor weighs 165g only.

Sharp and distinct edges, presenting a
dynamic beauty.
Craftsmanship
Manual winding, high groove full rate effectively reduces resistance,
lower motor temperature rise and higher efficiency
Excellent Material Selection,
Outstanding Performance
Silicon steel sheets imported from
Kawasaki, Japan are punched into high
-performance iron cores
The efficiency
data is even better.
The magnetic circuit is
optimized for common
working conditions
200℃
high-temperature
resistant enameled wires.
Recommended Combinations
  • Motor
    M-6208-155KV
    Battery
    12S LiPo
  • Propeller
    MP21*6.3/ML22*7.8
    Thrust / rotor
    2~2.5kg
  • ESC
    XRotor Pro-H60A-14S
    Takeoff weight of quadrotor
    8~10kg
  • Motor
    M-6208-310KV
    Battery
    6S LiPo
  • Propeller
    MP21*6.3/ML22*7.8
    Thrust / rotor
    2~2.5kg
  • ESC
    XRotor Pro-H60A-6S
    Takeoff weight of quadrotor
    8~10kg

M 6208  CAD
Model
M-6208-155KV M-6208-310KV
Specification
Battery(LiPo) 12S 6S
No-load current 0.92 1.65
Maximum current (Non-hermetic Ambient Temperature ≤ 25℃) 28.5 60
KV 155 310
Stator Size Φ61.5 Φ61.5
Motor Size Φ68.7*25.8 Φ68.7*25.8
Resistance 161.4 42.3
Slot& Pole 24N28P 24N28P
Bearing Water proof bearing Water proof bearing
Weight(With wire) 165 169
Props mounting dimensions 4×M3@D12+D18 4×M3@D12+D18
Motor mounting dimensions 4×M4@D32 4×M4@D32
Dynamic balance ≤8mg ≤8mg
Wire length Wire Size 50mm/enamelled wire outlet 50mm/enamelled wire outlet
Protection level IPX5 IPX5
Recommended application combinations
Motor M-6208-155KV M-6208-310KV
Propeller MP21*6.3/ML22*7.8 MP21*6.3/ML22*7.8
ESC XRotor Pro-H60A-14S XRotor Pro-H60A-6S
Battery 12S LiPo 6S LiPo
Takeoff weight / rotor 2~2.5Kg 2~2.5Kg
Takeoff weight of quadrotor 8~10Kg 8~10Kg
M 6208 155KV+21*6.3" Load performance parameters
M 6208 155KV+21*6.3" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

EEfficiency(g/W)

Torque(N-m)

Temperature(℃)

46V (12S LiPo)

21*6.3"

33%

853

1.5

67.7

2152

12.6

0.22

58°C

35%

953

1.7

77.8

2249

12.2

0.24

37%

1075

2.0

90.2

2363

11.9

0.27

39%

1212

2.3

104.6

2487

11.6

0.31

42%

1440

2.8

129.2

2680

11.1

0.37

45%

1683

3.4

157.2

2875

10.7

0.42

48%

1934

4.1

188.1

3065

10.3

0.49

51%

2185

4.8

221.7

3246

9.9

0.55

54%

2436

5.6

257.7

3420

9.5

0.61

57%

2684

6.4

296.1

3585

9.1

0.67

60%

2931

7.3

336.7

3743

8.7

0.73

63%

3178

8.2

379.8

3896

8.4

0.79

66%

3428

9.2

425.8

4046

8.1

0.85

69%

3684

10.3

475.0

4192

7.8

0.92

72%

3949

11.5

528.1

4337

7.5

0.98

75%

4225

12.7

585.5

4480

7.2

1.05

78%

4512

14.1

647.4

4621

7.0

1.13

81%

4812

15.5

714.2

4760

6.7

1.20

84%

5121

17.1

785.7

4896

6.5

1.28

87%

5435

18.7

861.4

5028

6.3

1.36

90%

5748

20.4

940.3

5157

6.1

1.44

100%

6582

25.6

1180.0

5536

5.6

1.65

Under the environment of sea level altitude, the data above is measured in room temperature of 25°C.The throttle input is able to adjust the tension, and the motor temperature is the temperature of the rated throttle running for 10 minutes.
M 6208 155kv+22*7.8" Load performance parameters
M 6208 155kv+22*7.8" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

EEfficiency(g/W)

Torque(N-m)

Temperature(℃)

46V (12S LiPo)

22*7.8"

33%

1030

1.7

77.2

2101

13.3

0.29

79°C

35%

1132

1.9

87.5

2195

12.9

0.31

37%

1258

2.2

100.5

2307

12.5

0.35

39%

1402

2.5

116.0

2429

12.1

0.38

42%

1641

3.1

143.2

2622

11.5

0.45

45%

1900

3.8

174.8

2816

10.9

0.51

48%

2168

4.6

210.1

3004

10.3

0.58

51%

2440

5.4

248.5

3184

9.8

0.65

54%

2712

6.3

289.7

3353

9.4

0.72

57%

2981

7.2

333.2

3514

8.9

0.79

60%

3249

8.2

379.1

3666

8.6

0.86

63%

3516

9.3

427.3

3812

8.2

0.93

66%

3784

10.4

478.3

3953

7.9

1.00

69%

4056

11.6

532.4

4091

7.6

1.07

72%

4334

12.8

590.2

4226

7.3

1.15

75%

4619

14.2

652.4

4361

7.1

1.22

78%

4915

15.6

719.5

4494

6.8

1.30

81%

5220

17.2

792.0

4625

6.6

1.38

84%

5534

18.9

870.2

4755

6.4

1.46

87%

5852

20.7

953.8

4880

6.1

1.54

90%

6171

22.6

1042.2

5000

5.9

1.63

100%

7062

28.7

1323.1

5317

5.3

1.87

Under the environment of sea level altitude, the data above is measured in room temperature of 25°C.The throttle input is able to adjust the tension, and the motor temperature is the temperature of the rated throttle running for 10 minutes.
M 6208 310kv+21*6.3" Load performance parameters
M 6208 310kv+21*6.3" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

EEfficiency(g/W)

Torque(N-m)

Temperature(℃)

46V (12S LiPo)

21*6.3"

33%

1038

3.8

87.7

2588

11.8

0.25

55°C

35%

1157

4.3

98.7

2714

11.7

0.28

37%

1273

4.8

111.3

2836

11.4

0.30

39%

1388

5.4

125.2

2955

11.1

0.33

42%

1560

6.4

147.9

3128

10.5

0.37

45%

1732

7.5

172.5

3295

10.0

0.41

48%

1906

8.6

198.8

3457

9.6

0.45

51%

2084

9.8

226.3

3613

9.2

0.50

54%

2265

11.1

255.1

3764

8.9

0.54

57%

2449

12.4

285.1

3909

8.6

0.58

60%

2638

13.7

316.3

4050

8.3

0.63

63%

2830

15.1

348.9

4186

8.1

0.67

66%

3026

16.6

383.1

4319

7.9

0.72

69%

3226

18.2

419.3

4450

7.7

0.76

72%

3428

19.9

457.9

4580

7.5

0.81

75%

3635

21.7

499.3

4711

7.3

0.86

78%

3845

23.6

544.1

4844

7.1

0.91

81%

4060

25.7

592.6

4981

6.9

0.96

84%

4282

28.0

645.3

5123

6.6

1.01

87%

4512

30.5

702.5

5270

6.4

1.07

90%

4754

33.1

764.0

5420

6.2

1.13

100%

5634

41.9

965.1

5837

5.8

1.34

Under the environment of sea level altitude, the data above is measured in room temperature of 25°C.The throttle input is able to adjust the tension, and the motor temperature is the temperature of the rated throttle running for 10 minutes.
M 6208 310kv+22*7.8" Load performance parameters
M 6208 310kv+22*7.8" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

EEfficiency(g/W)

Torque(N-m)

Temperature(℃)

23V(6S LiPo)

22*7.8"

33%

1399

5.1

118.1

2465

11.8

0.37

83.0°C

35%

1528

5.8

133.0

2572

11.5

0.40

37%

1666

6.5

150.2

2682

11.1

0.44

39%

1809

7.4

169.5

2793

10.7

0.48

42%

2031

8.8

201.8

2957

10.1

0.54

45%

2259

10.3

237.3

3116

9.5

0.60

48%

2488

11.9

275.0

3268

9.0

0.66

51%

2716

13.6

314.3

3411

8.6

0.72

54%

2943

15.4

354.8

3546

8.3

0.78

57%

3167

17.2

396.2

3674

8.0

0.84

60%

3390

19.0

438.7

3795

7.7

0.89

63%

3613

20.9

482.4

3912

7.5

0.95

66%

3837

22.9

527.9

4026

7.3

1.01

69%

4064

25.0

575.8

4139

7.1

1.07

72%

4297

27.2

626.7

4252

6.9

1.13

75%

4537

29.6

681.5

4366

6.7

1.19

78%

4787

32.2

741.4

4484

6.5

1.26

81%

5049

35.0

807.2

4605

6.3

1.33

84%

5324

38.2

880.2

4732

6.0

1.40

87%

5614

41.7

961.3

4863

5.8

1.48

90%

5919

45.6

1051.2

4997

5.6

1.56

100%

6977

60.4

1390.7

5399

5.0

1.86

Under the environment of sea level altitude, the data above is measured in room temperature of 25°C.The throttle input is able to adjust the tension, and the motor temperature is the temperature of the rated throttle running for 10 minutes.
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FAQ

M 6208 UL
6208-155KV/310KV
Industrial-level Multi-rotor UAV Motor
Reliable and Efficient, Ideal for Long Endurance.
Designed for high-end industrial-grade multi-rotor drone applications. It is widely used in aerial photography, surveying, monitoring, inspection, public safety and other scenarios.
The Sharp and Distinct Edges Stands Out Remarkably
The rotor is well balanced, featuring an ultimate hollow design for maximum weight reduction. The motor weighs 165g only.

Sharp and distinct edges, presenting a dynamic beauty.
Craftsmanship
Manual winding, high groove full rate effectively reduces resistance, lower motor temperature rise and higher efficiency
M 6208  CAD
Model
M-6208-155KV M-6208-310KV
Specification
Battery(LiPo) 12S 6S
No-load current 0.92 1.65
Maximum current (Non-hermetic Ambient Temperature ≤ 25℃) 28.5 60
KV 155 310
Stator Size Φ61.5 Φ61.5
Motor Size Φ68.7*25.8 Φ68.7*25.8
Resistance 161.4 42.3
Slot& Pole 24N28P 24N28P
Bearing Water proof bearing Water proof bearing
Weight(With wire) 165 169
Props mounting dimensions 4×M3@D12+D18 4×M3@D12+D18
Motor mounting dimensions 4×M4@D32 4×M4@D32
Dynamic balance ≤8mg ≤8mg
Wire length Wire Size 50mm/enamelled wire outlet 50mm/enamelled wire outlet
Protection level IPX5 IPX5
Recommended application combinations
Motor M-6208-155KV M-6208-310KV
Propeller MP21*6.3/ML22*7.8 MP21*6.3/ML22*7.8
ESC XRotor Pro-H60A-14S XRotor Pro-H60A-6S
Battery 12S LiPo 6S LiPo
Takeoff weight / rotor 2~2.5Kg 2~2.5Kg
Takeoff weight of quadrotor 8~10Kg 8~10Kg
M 6208 155KV+21*6.3" Load performance parameters
M 6208 155KV+21*6.3" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

EEfficiency(g/W)

Torque(N-m)

Temperature(℃)

46V (12S LiPo)

21*6.3"

33%

853

1.5

67.7

2152

12.6

0.22

58°C

35%

953

1.7

77.8

2249

12.2

0.24

37%

1075

2.0

90.2

2363

11.9

0.27

39%

1212

2.3

104.6

2487

11.6

0.31

42%

1440

2.8

129.2

2680

11.1

0.37

45%

1683

3.4

157.2

2875

10.7

0.42

48%

1934

4.1

188.1

3065

10.3

0.49

51%

2185

4.8

221.7

3246

9.9

0.55

54%

2436

5.6

257.7

3420

9.5

0.61

57%

2684

6.4

296.1

3585

9.1

0.67

60%

2931

7.3

336.7

3743

8.7

0.73

63%

3178

8.2

379.8

3896

8.4

0.79

66%

3428

9.2

425.8

4046

8.1

0.85

69%

3684

10.3

475.0

4192

7.8

0.92

72%

3949

11.5

528.1

4337

7.5

0.98

75%

4225

12.7

585.5

4480

7.2

1.05

78%

4512

14.1

647.4

4621

7.0

1.13

81%

4812

15.5

714.2

4760

6.7

1.20

84%

5121

17.1

785.7

4896

6.5

1.28

87%

5435

18.7

861.4

5028

6.3

1.36

90%

5748

20.4

940.3

5157

6.1

1.44

100%

6582

25.6

1180.0

5536

5.6

1.65

Under the environment of sea level altitude, the data above is measured in room temperature of 25°C.The throttle input is able to adjust the tension, and the motor temperature is the temperature of the rated throttle running for 10 minutes.
M 6208 155kv+22*7.8" Load performance parameters
M 6208 155kv+22*7.8" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

EEfficiency(g/W)

Torque(N-m)

Temperature(℃)

46V (12S LiPo)

22*7.8"

33%

1030

1.7

77.2

2101

13.3

0.29

79°C

35%

1132

1.9

87.5

2195

12.9

0.31

37%

1258

2.2

100.5

2307

12.5

0.35

39%

1402

2.5

116.0

2429

12.1

0.38

42%

1641

3.1

143.2

2622

11.5

0.45

45%

1900

3.8

174.8

2816

10.9

0.51

48%

2168

4.6

210.1

3004

10.3

0.58

51%

2440

5.4

248.5

3184

9.8

0.65

54%

2712

6.3

289.7

3353

9.4

0.72

57%

2981

7.2

333.2

3514

8.9

0.79

60%

3249

8.2

379.1

3666

8.6

0.86

63%

3516

9.3

427.3

3812

8.2

0.93

66%

3784

10.4

478.3

3953

7.9

1.00

69%

4056

11.6

532.4

4091

7.6

1.07

72%

4334

12.8

590.2

4226

7.3

1.15

75%

4619

14.2

652.4

4361

7.1

1.22

78%

4915

15.6

719.5

4494

6.8

1.30

81%

5220

17.2

792.0

4625

6.6

1.38

84%

5534

18.9

870.2

4755

6.4

1.46

87%

5852

20.7

953.8

4880

6.1

1.54

90%

6171

22.6

1042.2

5000

5.9

1.63

100%

7062

28.7

1323.1

5317

5.3

1.87

Under the environment of sea level altitude, the data above is measured in room temperature of 25°C.The throttle input is able to adjust the tension, and the motor temperature is the temperature of the rated throttle running for 10 minutes.
M 6208 310kv+21*6.3" Load performance parameters
M 6208 310kv+21*6.3" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

EEfficiency(g/W)

Torque(N-m)

Temperature(℃)

46V (12S LiPo)

21*6.3"

33%

1038

3.8

87.7

2588

11.8

0.25

55°C

35%

1157

4.3

98.7

2714

11.7

0.28

37%

1273

4.8

111.3

2836

11.4

0.30

39%

1388

5.4

125.2

2955

11.1

0.33

42%

1560

6.4

147.9

3128

10.5

0.37

45%

1732

7.5

172.5

3295

10.0

0.41

48%

1906

8.6

198.8

3457

9.6

0.45

51%

2084

9.8

226.3

3613

9.2

0.50

54%

2265

11.1

255.1

3764

8.9

0.54

57%

2449

12.4

285.1

3909

8.6

0.58

60%

2638

13.7

316.3

4050

8.3

0.63

63%

2830

15.1

348.9

4186

8.1

0.67

66%

3026

16.6

383.1

4319

7.9

0.72

69%

3226

18.2

419.3

4450

7.7

0.76

72%

3428

19.9

457.9

4580

7.5

0.81

75%

3635

21.7

499.3

4711

7.3

0.86

78%

3845

23.6

544.1

4844

7.1

0.91

81%

4060

25.7

592.6

4981

6.9

0.96

84%

4282

28.0

645.3

5123

6.6

1.01

87%

4512

30.5

702.5

5270

6.4

1.07

90%

4754

33.1

764.0

5420

6.2

1.13

100%

5634

41.9

965.1

5837

5.8

1.34

Under the environment of sea level altitude, the data above is measured in room temperature of 25°C.The throttle input is able to adjust the tension, and the motor temperature is the temperature of the rated throttle running for 10 minutes.
M 6208 310kv+22*7.8" Load performance parameters
M 6208 310kv+22*7.8" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

EEfficiency(g/W)

Torque(N-m)

Temperature(℃)

23V(6S LiPo)

22*7.8"

33%

1399

5.1

118.1

2465

11.8

0.37

83.0°C

35%

1528

5.8

133.0

2572

11.5

0.40

37%

1666

6.5

150.2

2682

11.1

0.44

39%

1809

7.4

169.5

2793

10.7

0.48

42%

2031

8.8

201.8

2957

10.1

0.54

45%

2259

10.3

237.3

3116

9.5

0.60

48%

2488

11.9

275.0

3268

9.0

0.66

51%

2716

13.6

314.3

3411

8.6

0.72

54%

2943

15.4

354.8

3546

8.3

0.78

57%

3167

17.2

396.2

3674

8.0

0.84

60%

3390

19.0

438.7

3795

7.7

0.89

63%

3613

20.9

482.4

3912

7.5

0.95

66%

3837

22.9

527.9

4026

7.3

1.01

69%

4064

25.0

575.8

4139

7.1

1.07

72%

4297

27.2

626.7

4252

6.9

1.13

75%

4537

29.6

681.5

4366

6.7

1.19

78%

4787

32.2

741.4

4484

6.5

1.26

81%

5049

35.0

807.2

4605

6.3

1.33

84%

5324

38.2

880.2

4732

6.0

1.40

87%

5614

41.7

961.3

4863

5.8

1.48

90%

5919

45.6

1051.2

4997

5.6

1.56

100%

6977

60.4

1390.7

5399

5.0

1.86

Under the environment of sea level altitude, the data above is measured in room temperature of 25°C.The throttle input is able to adjust the tension, and the motor temperature is the temperature of the rated throttle running for 10 minutes.
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