M 4006 HP/UL
Industrial Multirotor Drone Motors HP & ULSeries -330KV/350KV

High Efficiency,
Long Endurance
  • The recommended
    thrust is
    1Kg
  • Takeoff weight of
    quadrotor 4.0Kg
Excellent Design
Produced using industry-level motor technology,
which requires high grade raw materials,
better tolerances, to provide reliability and performance.

It adopts a new shape design of the rotor
that stands out from the other motors in the market.

Knurled shaft design to provide tigher tolerances.

The new magnetic circuit design optimizes the anti-emotive
force harmonics, that produce a higher sine wave.
and is better matched with the ESC.
Excellent Design for Eenhanced Protection
Produced using industry-level motor technology,
which has higher specifications and requires high grade raw materials,
better tolerances, to provide reliability and performance.

Brand new exterior design, optimized fan ports,
effectively improving the protection level.

The end of the rotor bracket is left to avoid air
contact with the edge of the propeller root.
Knurled shaft design to provide tigher tolerances.

The rotor bracket adopts a centrifugal fan heat dissipation
structure to effectively improve the heat dissipation capacity.

The new magnetic circuit design optimizes the anti-emotive
force harmonics, that produce a higher sine wave
and is better matched with the ESC.
  • UL
  • HP
Attention to Detail,
Stable and Reliable!
Extreme weight reduction, integrated design of stator seat
and back cover, optimizing the required parts.
The tail of the main shaft uses a snap ring and locking screw structure
to enhance the reliability of the motor
with high-quality anti-rust screws to ensure that the rotor is foolproof.
Attention to Detail,
Extremely Lightweight!
The tail of the spindle uses a snap ring and locking screw structure
to enhance the reliability of the motor
with high-quality anti-rust screws to ensure the rotor is secure.
  • UL
  • HP
Adopts High Quality Materials

High-quality bearings

low friction torque,
extending the lifespan of the motor

Main shaft

high toughness carbide

High-performance iron core

0.2mm low-loss silicon steel
sheet punched

The outer rotor casing

made of 20# seamless steel tube with nickel
electrophoresis design, which has excellent
conductivity and corrosion resistance.
Recommended
Combinations
  • Motor
    M-4006-UL

    Battery
    6S LiPo
  • Propeller
    MP16*5.4"

    Thrust/rotor
    0.6~1.0kg
  • ESC
    XRotor Pro-H40A-6S
    XRotor Pro-H60A-6S
    Takeoff weight of quadrotor
    2.4~4.0kg
  • Motor
    M-4006-HP
    Battery
    6S LiPo
  • Propeller
    MP16*5.4"
    MP17*5.8"
    Thrust/rotor
    0.6~1.0kg
  • ESC
    XRotor Pro-H40A-6S
    XRotor Pro-H60A-6S
    Takeoff weight of quadrotor
    2.4~4.0kg
M 4006 HP CAD
M 4006 UL CAD
Model
M 4006 330KV HP M 4006 350KV UL
Specification
Motor Size Φ44.4*H19.7mm Φ44.4*H19.3mm
Stator Size Φ39mm Φ39mm
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
Enamelled wire 220℃ 220℃
Magnet 180℃ 180℃
Isolation test 500V AC high voltage resistance test 500V AC high voltage resistance test
Protection level IP45 IPX5
Slot& Pole 18N 24P 18N 24P
Dynamic balance ≤5mg ≤5mg
Bearing Water proof bearing Water proof bearing
Motor axle diameter Φ4mm Φ4mm
Props mounting dimensions 4×M3@D12 4×M3@D12
Motor mounting dimensions 4×M3@D25 4×M3@D25
KV 330 350
Battery(LiPo) LiPo-6S LiPo-6S
No-load current 0.58 A 0.64 A
Maximum current (Non-hermetic Ambient Temperature ≤ 25℃） 15.8 A 17.3 A
Max power 363 W 358 W
Max thrust 2.3 kg 2.5 kg
Resistance 218.5mΩ 209.7mΩ
Wire Size enamelled wire outlet enamelled wire outlet
Wire length 50 mm 60 mm
Weight（With wire） 72g 66.1g
Recommended application combinations
Motor M-4006-HP M-4006-UL
Propeller MP16*5.4"/MP17*5.8" MP16*5.4"
ESC XRotor Pro-H40A-6S/XRotor Pro-H60A-6S XRotor Pro-H40A-6S/XRotor Pro-H60A-6S
Battery 6S LiPo 6S LiPo
Thrust/rotor 0.6~1.0kg 0.6~1.0kg
Takeoff weight of quadrotor 2.4~4.0kg 2.4~4.0kg
M 4006 HP 330KV+MP 16*5.4" Load performance parameters
M 4006 HP 330KV+MP 16*5.4" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature(℃)

23V (6S LiPo)

MP 16*5.4"

33%

300

0.8

18.9

2163

15.8

0.06

57.0°C

35%

329

0.9

21.3

2252

15.4

0.07

37%

361

1.0

24.1

2348

15.0

0.07

39%

398

1.2

27.4

2452

14.5

0.08

42%

458

1.4

33.0

2618

13.9

0.09

45%

527

1.7

39.8

2794

13.2

0.10

48%

601

2.1

47.6

2976

12.6

0.12

51%

681

2.5

56.5

3159

12.1

0.13

54%

766

2.9

66.4

3342

11.5

0.15

57%

853

3.4

77.3

3521

11.0

0.17

60%

944

3.9

89.0

3696

10.6

0.18

63%

1035

4.4

101.6

3864

10.2

0.20

66%

1127

5.0

115.0

4025

9.8

0.22

69%

1218

5.6

128.9

4179

9.4

0.23

72%

1308

6.2

143.5

4326

9.1

0.25

75%

1397

6.9

158.5

4466

8.8

0.27

78%

1484

7.6

173.9

4599

8.5

0.28

81%

1571

8.3

189.9

4726

8.3

0.30

84%

1656

9.0

206.5

4849

8.0

0.32

87%

1743

9.7

223.9

4971

7.8

0.33

90%

1831

10.5

242.4

5092

7.6

0.35

100%

2154

13.7

315.2

5516

6.8

0.41
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 4006 HP 330KV+MP 17*5.8" Load performance parameters
M 4006 HP 330KV+MP 17*5.8" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature(℃)

23V (6S LiPo)

MP 17*5.8"

33%

356

1.0

22.3

2105

16.0

0.07

70°C

35%

394

1.1

25.6

2205

15.4

0.08

37%

436

1.3

29.5

2311

14.8

0.09

39%

482

1.5

33.8

2423

14.3

0.10

42%

557

1.8

41.1

2594

13.6

0.11

45%

639

2.1

49.4

2767

12.9

0.13

48%

724

2.6

58.8

2938

12.3

0.15

51%

813

3.0

69.2

3105

11.7

0.17

54%

903

3.5

80.7

3268

11.2

0.18

57%

995

4.0

93.1

3426

10.7

0.20

60%

1086

4.6

106.4

3579

10.2

0.22

63%

1178

5.2

120.4

3726

9.8

0.24

66%

1269

5.9

135.1

3869

9.4

0.26

69%

1360

6.5

150.3

4006

9.0

0.27

72%

1450

7.2

166.1

4138

8.7

0.29

75%

1539

7.9

182.5

4265

8.4

0.31

78%

1629

8.7

199.5

4388

8.2

0.33

81%

1719

9.4

217.2

4506

7.9

0.34

84%

1809

10.3

235.8

4620

7.7

0.36

87%

1902

11.1

255.6

4731

7.4

0.38

90%

1997

12.1

277.0

4840

7.2

0.40

100%

2331

15.8

363.6

5177

6.4

0.47
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 4006 UL 350KV+MP 16*5.4" Load performance parameters
M 4006 UL 350KV+MP 16*5.4" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature(℃)

23V (6S LiPo)

MP 16*5.4"

33%

347

1.0

23.2

2320

15.0

0.07

71.2°C

35%

374

1.1

25.9

2400

14.4

0.07

37%

410

1.3

29.5

2503

13.9

0.08

39%

482

1.5

33.8

2423

14.3

0.10

42%

557

1.8

41.1

2594

13.6

0.11

45%

639

2.1

49.4

2767

12.9

0.13

48%

724

2.6

59.9

3209

11.7

0.14

51%

793

3.1

70.7

3399

11.2

0.15

54%

885

3.6

82.5

3583

10.7

0.17

57%

976

4.1

95.1

3758

10.3

0.19

60%

1066

4.7

108.5

3926

9.8

0.20

63%

1154

5.3

122.6

4087

9.4

0.22

66%

1242

6.0

137.4

4241

9.0

0.24

69%

1329

6.6

152.9

4389

8.7

0.26

72%

1417

7.3

169.1

4532

8.4

0.27

75%

1506

8.1

186.2

4670

8.1

0.29

78%

1595

8.9

204.2

4803

7.8

0.31

81%

1687

9.7

223.2

4931

7.6

0.32

84%

1781

10.6

243.3

5053

7.3

0.34

87%

1876

11.5

264.3

5170

71

0.36

90%

1971

12.4

286.3

5283

6.9

0.37

100%

2251

15.6

357.8

5618

6.3

0.43
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 4006 HP Load performance parameters
M 4006 UL Load performance parameters
M 4006 UL 3D Model Drawing
M 4006 HP 3D Model Drawing
M 4006 UL CAD
M 4006 HP CAD
M 4006 HP Specification
M 4006 UL Specification

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M 4006 HP/UL
Overview Specifications Support Accessories Detail Contact us Shop
Industrial Multirotor Drone Motors
HP & UL Series-330KV/350KV
High efficiency, long endurance
  • The recommended
    thrust is 1Kg
  • Takeoff weight of
    quadrotor 4.0Kg
Excellent design
Produced using industry-level motor technology, which requires high grade raw materials, better tolerances, to provide reliability and performance.

It adopts a new shape design of the rotor that stands out from the other motors in the market.

Knurled shaft design to provide tigher tolerances.

The new magnetic circuit design optimizes the anti-emotiv force harmonics, that produce a higher sine wave. and is better matched with the ESC.
Excellent design for
enhanced protection
Produced using industry-level motor technology,
which has higher specifications and requires high grade raw materials,
better tolerances, to provide reliability and performance.

Brand new exterior design, optimized fan ports,
effectively improving the protection level.

The end of the rotor bracket is left to avoid air
contact with the edge of the propeller root.
Knurled shaft design to provide tigher tolerances.

The rotor bracket adopts a centrifugal fan heat dissipation
structure to effectively improve the heat dissipation capacity.

The new magnetic circuit design optimizes the anti-emotive
force harmonics, that produce a higher sine wave
and is better matched with the ESC.
  • UL
  • HP
Attention to detail, stable and reliable!
Extreme weight reduction, integrated design of stator seat and back cover, optimizing the required parts. The tail of the main shaft uses a snap ring and locking screw structure to enhance the reliability of the motor with high-quality anti-rust screws to ensure that the rotor is foolproof.
Attention to detail, extremely lightweight!
The tail of the spindle uses a snap ring and locking screw structure to enhance the reliability of the motor with high-quality anti-rust screws to ensure the rotor is secure.
  • UL
  • HP
Recommended
combinations
M 4006 HP CAD
M 4006 UL CAD
Model
M 4006 330KV HP M 4006 350KV UL
Specification
Motor Size Φ44.4*H19.7mm Φ44.4*H19.3mm
Stator Size Φ39mm Φ39mm
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
Enamelled wire 220℃ 220℃
Magnet 180℃ 180℃
Isolation test 500V AC high voltage resistance test 500V AC high voltage resistance test
Protection level IP45 IPX5
Slot& Pole 18N 24P 18N 24P
Dynamic balance ≤5mg ≤5mg
Bearing Water proof bearing Water proof bearing
Motor axle diameter Φ4mm Φ4mm
Props mounting dimensions 4×M3@D12 4×M3@D12
Motor mounting dimensions 4×M3@D25 4×M3@D25
KV 330 350
Battery(LiPo) LiPo-6S LiPo-6S
No-load current 0.58 A 0.64 A
Maximum current (Non-hermetic Ambient Temperature ≤ 25℃） 15.8 A 17.3 A
Max power 363 W 358 W
Max thrust 2.3 kg 2.5 kg
Resistance 218.5mΩ 209.7mΩ
Wire Size enamelled wire outlet enamelled wire outlet
Wire length 50 mm 60 mm
Weight（With wire） 72g 66.1g
Recommended application combinations
Motor M-4006-HP M-4006-UL
Propeller MP16*5.4"/MP17*5.8" MP16*5.4"
ESC XRotor Pro-H40A-6S/XRotor Pro-H60A-6S XRotor Pro-H40A-6S/XRotor Pro-H60A-6S
Battery 6S LiPo 6S LiPo
Thrust/rotor 0.6~1.0kg 0.6~1.0kg
Takeoff weight of quadrotor 2.4~4.0kg 2.4~4.0kg
M 4006 HP 330KV+MP 16*5.4" Load performance parameters
M 4006 HP 330KV+MP 16*5.4" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature(℃)

23V (6S LiPo)

MP 16*5.4"

33%

300

0.8

18.9

2163

15.8

0.06

57.0°C

35%

329

0.9

21.3

2252

15.4

0.07

37%

361

1.0

24.1

2348

15.0

0.07

39%

398

1.2

27.4

2452

14.5

0.08

42%

458

1.4

33.0

2618

13.9

0.09

45%

527

1.7

39.8

2794

13.2

0.10

48%

601

2.1

47.6

2976

12.6

0.12

51%

681

2.5

56.5

3159

12.1

0.13

54%

766

2.9

66.4

3342

11.5

0.15

57%

853

3.4

77.3

3521

11.0

0.17

60%

944

3.9

89.0

3696

10.6

0.18

63%

1035

4.4

101.6

3864

10.2

0.20

66%

1127

5.0

115.0

4025

9.8

0.22

69%

1218

5.6

128.9

4179

9.4

0.23

72%

1308

6.2

143.5

4326

9.1

0.25

75%

1397

6.9

158.5

4466

8.8

0.27

78%

1484

7.6

173.9

4599

8.5

0.28

81%

1571

8.3

189.9

4726

8.3

0.30

84%

1656

9.0

206.5

4849

8.0

0.32

87%

1743

9.7

223.9

4971

7.8

0.33

90%

1831

10.5

242.4

5092

7.6

0.35

100%

2154

13.7

315.2

5516

6.8

0.41
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 4006 HP 330KV+MP 17*5.8" Load performance parameters
M 4006 HP 330KV+MP 17*5.8" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature(℃)

23V (6S LiPo)

MP 17*5.8"

33%

356

1.0

22.3

2105

16.0

0.07

70°C

35%

394

1.1

25.6

2205

15.4

0.08

37%

436

1.3

29.5

2311

14.8

0.09

39%

482

1.5

33.8

2423

14.3

0.10

42%

557

1.8

41.1

2594

13.6

0.11

45%

639

2.1

49.4

2767

12.9

0.13

48%

724

2.6

58.8

2938

12.3

0.15

51%

813

3.0

69.2

3105

11.7

0.17

54%

903

3.5

80.7

3268

11.2

0.18

57%

995

4.0

93.1

3426

10.7

0.20

60%

1086

4.6

106.4

3579

10.2

0.22

63%

1178

5.2

120.4

3726

9.8

0.24

66%

1269

5.9

135.1

3869

9.4

0.26

69%

1360

6.5

150.3

4006

9.0

0.27

72%

1450

7.2

166.1

4138

8.7

0.29

75%

1539

7.9

182.5

4265

8.4

0.31

78%

1629

8.7

199.5

4388

8.2

0.33

81%

1719

9.4

217.2

4506

7.9

0.34

84%

1809

10.3

235.8

4620

7.7

0.36

87%

1902

11.1

255.6

4731

7.4

0.38

90%

1997

12.1

277.0

4840

7.2

0.40

100%

2331

15.8

363.6

5177

6.4

0.47
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 4006 UL 350KV+MP 16*5.4" Load performance parameters
M 4006 UL 350KV+MP 16*5.4" Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature(℃)

23V (6S LiPo)

MP 16*5.4"

33%

347

1.0

23.2

2320

15.0

0.07

71.2°C

35%

374

1.1

25.9

2400

14.4

0.07

37%

410

1.3

29.5

2503

13.9

0.08

39%

482

1.5

33.8

2423

14.3

0.10

42%

557

1.8

41.1

2594

13.6

0.11

45%

639

2.1

49.4

2767

12.9

0.13

48%

724

2.6

59.9

3209

11.7

0.14

51%

793

3.1

70.7

3399

11.2

0.15

54%

885

3.6

82.5

3583

10.7

0.17

57%

976

4.1

95.1

3758

10.3

0.19

60%

1066

4.7

108.5

3926

9.8

0.20

63%

1154

5.3

122.6

4087

9.4

0.22

66%

1242

6.0

137.4

4241

9.0

0.24

69%

1329

6.6

152.9

4389

8.7

0.26

72%

1417

7.3

169.1

4532

8.4

0.27

75%

1506

8.1

186.2

4670

8.1

0.29

78%

1595

8.9

204.2

4803

7.8

0.31

81%

1687

9.7

223.2

4931

7.6

0.32

84%

1781

10.6

243.3

5053

7.3

0.34

87%

1876

11.5

264.3

5170

71

0.36

90%

1971

12.4

286.3

5283

6.9

0.37

100%

2251

15.6

357.8

5618

6.3

0.43
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 4006 HP Load performance parameters
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