FM6510 drone motor for Multicopter Strong Power UAV

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM6510 KV130

40A
(6S-14S)

P2270

22 inch 

Multi-rotor
drone,VTOL

2.0KG-2.5KG
uniaxial

5.96KG

995W

Load test data

Lithium Battery :12S      44.4V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficiency

(g/W)

Torque
(N.m)

Accelerator

44.18

896

1.32

2066

58.32

15.36

0.27

40%

44.18

1370

2.45

2364

108.24

12.66

0.44

45%

44.17

1645

3.14

2569

138.69

11.86

0.52

50%

44.15

1965

4.11

2788

181.46

10.83

0.62

55%

44.14

2294

5.12

3027

226.00

10.15

0.71

60%

44.13

2683

6.38

3261

281.55

9.53

0.82

65%

44.14

2998

7.73

3483

341.20

8.79

0.94

70%

44.10

3321

9.03

3668

398.22

8.34

1.04

75%

44.09

3705

10.58

3866

466.47

7.94

1.15

80%

44.08

3974

12.15

4065

535.57

7.42

1.26

85%

44.05

4396

14.31

4269

630.36

6.97

1.41

90%

43.99

4824

16.36

4447

719.68

6.70

1.55

95%

43.98

5172

18.5

4625

813.63

6.36

1.68

100%

Load test data

Lithium Battery :12S 48V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficiency

(g/W)

Torque
(N.m)

Accelerat
Or

47.76

1323

2.1

2304

100.30

13.19

0.42

40%

47.78

1573

2.71

2505

129.48

12.15

0.49

45%

47.77

1867

3.48

2727

166.24

11.23

0.58

50%

47.77

2219

4.56

2984

217.83

10.19

0.70

55%

47.74

2631

5.74

3236

274.03

9.60

0.81

60%

47.71

3060

7.12

3478

339.70

9.01

0.93

65%

47.72

3370

8.54

3693

407.53

8.27

1.05

70%

47.69

3654

9.82

3910

468.32

7.80

1.14

75%

47.63

4129

11.57

4102

551.08

7.49

1.28

80%

47.63

4613

13.87

4296

660.63

6.98

1.47

85%

47.63

5085

16.05

4484

764.46

6.65

1.63

90%

47.58

5542

18.31

4664

871.19

6.36

1.78

95%

47.56

5966

20.93

4817

995.43

5.99

1.97

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max Thrust

Max power

FM6510 KV130

40A
(6S-14S)

P2480

Multi-rotor
drone

2.2KG-2.9KG
uniaxial

6.6KG

1259W

Load test data

Lithium Battery :12S      44.4V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

accelerat
Or

44.18

1550

2.67

2033

117.96

13.14

0.55

40%

44.19

1841

3.49

2233

154.22

11.94

0.66

45%

44.15

2152

4.38

2416

193.38

11.13

0.76

50%

44.14

2535

5.59

2609

246.74

10.27

0.90

55%

44.11

2946

7.08

2813

312.30

9.43

1.06

60%

44.09

345

8.88

3002

391.52

8.81

1.25

65%

44.07

3886

10.7

3185

471.55

8.24

1.41

70%

44.07

4256

12.55

3350

553.08

7.70

1.58

75%

44.05

4683

14.64

3505

644.89

7.26

1.76

80%

43.99

5126

16.94

3641

745.19

6.88

1.95

85%

43.93

5551

19.38

3770

851.36

6.52

2.16

90%

43.93

5866

22.03

3908

967.78

6.06

2.36

95%

43.92

6093

24.24

4050

1064.62

5.72

2.51

100%

Load test data

Lithium Battery :12S   48V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

Accelerat
Or

47.76

1750

2.96

2151

141.37

12.38

0.63

40%

47.77

2097

3.85

2339

183.91

11.40

0.75

45%

47.73

2447

4.87

2528

232.45

10.53

0.88

50%

47.74

2849

6.26

2755

298.85

9.53

1.04

55%

47.71

3289

7.82

2965

373.09

8.82

1.20

60%

47.70

3753

9.73

3165

464.12

8.09

1.40

65%

47.67

4211

11.62

3348

553.93

7.60

1.58

70%

47.66

4705

13.72

3505

653.90

7.20

1.78

75%

47.63

5003

15.58

3678

742.08

6.74

1.93

80%

47.59

5605

18.23

3809

867.57

6.46

2.18

85%

47.57

5892

20.75

3956

987.08

5.97

2.38

90%

47.53

6288

23.57

4074

1120.28

5.6

2.63

95%

47.49

6618

26.52

4165

1259.43

5.25

2.89

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM6510 KV130

40A
(6S-14S)

G2360
23 inch 

Multi-rotor
drone

2.1KG-2.6KG
uniaxial  

5.9KG

997W

Load test data

/Lithium Battery :12S      44.4V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

Accelerat
Or

44.17

1182

1.83

2162

80.83

14.62

0.36

40%

44.18

1422

2.49

2361

110.01

12.93

0.44

45%

44.18

1697

3.23

2567

142.70

11.89

0.53

50%

44.15

1997

3.97

2794

175.28

11.39

0.60

55%

44.14

2323

5.19

3036

229.09

10.14

0.72

60%

44.11

2697

6.41

3273

282.75

9.54

0.82

65%

44.11

3085

7.88

3480

347.59

8.88

0.95

70%

44.09

3447

9.21

3663

406.07

8.49

1.06

75%

44.08

3820

10.86

3861

478.71

7.98

1.18

80%

44.06

4169

12.56

4068

553.39

7.53

1.30

85%

44.03

4641

14.75

4246

649.44

7.15

1.46

90%

43.97

5015

16.84

4418

740.45

6.77

1.60

95%

43.99

5413

19.16

4578

842.85

6.42

1.76

100%

Load test data

Lithium Battery :12S        48V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

Accelerat
Or

47.77

1351

2.09

2297

99.84

13.53

0.42

40%

47.76

1606

2.56

2504

122.27

13.14

0.47

45%

47.79

1918

3.44

2715

164.40

11.67

0.58

50%

47.76

2288

4.53

2970

216.35

10.58

0.70

55%

47.75

2632

5.76

3230

275.04

9.57

0.81

60%

47.74

3028

7.19

3478

343.25

8.82

0.94

65%

47.69

3388

8.52

3685

406.32

8.34

1.05

70%

47.68

3807

10.16

3885

484.43

7.86

1.19

75%

47.67

4220

11.95

4087

569.66

7.41

1.33

80%

47.65

4650

13.94

4283

664.24

7.00

1.48

85%

47.61

5108

16.18

4469

770.33

6.63

1.65

90%

47.59

5517

18.55

4649

882.79

6.25

1.81

95%

47.58

5915

20.97

4813

997.75

5.93

1.98

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM6510 KV260

60A
(4S-6S)

P2270
22 inch 

Multi-rotor
drone

2.0KG-2.5KG
uniaxial  

5.6KG

973W

Load test data

Lithium Battery :6S      22.2V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

Accelerat
Or

21.91

1108

3.61

2108

79.10

14.01

0.36

40%

21.89

1336

4.8

2324

105.07

12.72

0.43

45%

21.87

1611

6.24

2546

136.47

11.80

0.51

50%

21.83

1932

8.14

2796

177.70

10.87

0.61

55%

21.81

2279

10.55

3037

230.10

9.90

0.72

60%

21.79

2649

13.08

3246

285.01

9.29

0.84

65%

21.74

3027

15.77

3436

342.84

8.83

0.95

70%

21.73

3282

18.42

3631

400.27

8.20

1.05

75%

21.69

3663

21.67

3836

470.02

7.79

1.17

80%

  21.64

4069

25.72

4011

556.58

7.31

1.33

85%

   21.58

4373

29.52

4194

637.04

6.86

1.45

90%

   21.55

4794

34.07

4358

734.21

6.53

1.61

95%

   21.52

5130

37.92

4506

816.04

6.29

1.73

100%

Load test data

Lithium Battery :6S        24V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

Accelerat
Or

23.71

1262

4.03

2249

95.55

13.21

0.41

40%

23.69

1503

5.3

2473

125.56

11.97

0.48

45%

23.68

1838

7.06

2726

167.18

10.99

0.59

50%

23.64

2219

9.36

2986

221.27

10.03

0.71

55%

23.61

2626

11.94

3232

281.90

9.32

0.83

60%

23.56

2971

14.55

3454

342.80

8.67

0.95

65%

23.57

3291

17.25

3648

406.58

8.09

1.06

70%

23.51

3744

20.68

3850

486.19

7.70

1.21

75%

23.47

4142

24.54

4047

575.95

7.19

1.36

80%

23.42

4516

28.39

4239

664.89

6.79

1.50

85%

23.37

4924

32.91

4415

769.11

6.40

1.66

90%

23.29

5322

37.46

4574

872.44

6.10

1.82

95%

23.23

5686

41.91

4717

973.57

5.84

1.97

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM6510 KV260

60A
(4S-6S)

G2360
23 inch 

Multi-rotor
drone

2.0KG-2.5KG
uniaxial

5.9KG

997W

Load test data

Lithium Battery :6S     22.2V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

Accelerat
Or

21.92

1113

3.72

2109

81.54

13.65

0.37

40%

21.89

1356

4.78

2325

104.63

12.96

0.43

45%

21.88

1627

6.18

2545

135.22

12.03

0.51

50%

21.87

1956

8.26

2791

180.65

10.83

0.62

55%

21.82

2309

10.55

3031

230.20

10.03

0.73

60%

21.80

2653

13.01

3244

283.62

9.35

0.83

65%

21.76

3000

15.78

3436

343.37

8.74

0.95

70%

21.70

3331

18.35

3622

398.20

8.37

1.05

75%

21.69

3701

21.99

3809

476.96

7.76

1.20

80%

21.62

4112

25.82

3997

558.23

7.37

1.33

85%

21.59

4481

29.89

4165

645.33

6.94

1.48

90%

21.55

4848

34.22

4337

737.44

6.57

1.62

95%

21.52

5144

38.25

4480

823.14

6.25

1.75

100%

Load test data

Lithium Battery :6S       24V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

Accelerat
Or

23.68

1277

3.96

2252

93.77

13.62

0.40

40%

23.69

1544

5.35

2476

126.74

12.18

0.49

45%

23.67

1833

7.03

2731

166.40

11.02

0.58

50%

23.65

2208

9.27

2989

219.24

10.07

0.70

55%

23.61

2685

12.15

3225

286.86

9.36

0.85

60%

23.58

3053

14.86

3443

350.40

8.71

0.97

65%

23.56

3373

17.45

3639

411.12

8.20

1.08

70%

23.51

3679

20.98

3847

493.24

7.46

1.22

75%

23.45

4132

24.33

4047

570.54

7.24

1.35

80%

23.44

4520

28.45

4236

666.87

6.78

1.50

85%

23.35

5023

33.26

4397

776.62

6.47

1.69

90%

23.31

5371

37.88

4567

882.98

6.08

1.85

95%

23.25

5682

42.18

4713

980.69

5.79

1.99

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM6510 KV320

60A
(4S-6S)

P2070
20 inch  

Multi-rotor
drone

2.2KG-2.7KG
uniaxial  

5.8KG

1202W

load test data

Lithium Battery :6S 22.2V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

Accelerat
Or

21.90

1158

4.42

2697

96.80

11.9

0.34

40%

21.89

1430

6.06

3017

132.65

10.78

0.42

45%

21.85

1783

8.21

3364

179.39

9.94

0.51

50%

21.83

2139

10.65

3661

232.49

9.20

0.6

55%

21.79

2411

12.98

3942

282.83

8.52

0.69

60%

21.78

2760

15.92

4194

346.74

7.96

0.79

65%

21.71

3094

18.99

4447

412.27

7.50

0.89

70%

21.69

3458

22.95

4705

497.79

6.95

1.01

75%

21.64

3800

26.94

4940

582.98

6.52

1.13

80%

21.58

4184

31.68

5184

683.65

6.12

1.26

85%

21.53

4546

36.45

5416

784.77

5.79

1.38

90%

21.47

4925

41.46

5624

890.15

5.53

1.51

95%

21.43

5315

46.81

5822

1003.14

5.30

1.65

100%

Load test data

Lithium Battery :6S        24V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

Accelerat
Or

23.71

1295

5.02

2872

119.02

10.88

0.40

40%

23.67

1656

7.01

3230

165.93

9.98

0.49

45%

23.65

1998

9.44

3595

223.26

8.95

0.59

50%

23.61

2400

12.18

3888

287.57

8.35

0.71

55%

23.57

2762

15.11

4162

356.14

7.76

0.82

60%

23.55

3095

18.17

4440

427.90

7.23

0.92

65%

23.51

3436

21.68

4709

509.70

6.74

1.03

70%

23.45

3864

25.82

4971

605.48

6.38

1.16

75%

23.38

4249

30.22

5229

706.54

6.01

1.29

80%

23.32

4638

35.07

5482

817.83

5.67

1.42

85%

23.27

5084

40.64

5706

945.69

5.38

1.58

90%

23.21

5484

46.36

5917

1076.02

5.10

1.74

95%

23.14

5839

51.95

6123

1202.12

4.86

1.87

100%

Power configuration Measured date

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM6510 KV320

80A
(4S-6S)

P2270
22 inch 

Multi-rotor
drone

2.5KG-3.0KG
uniaxial

6.7KG

1506W

Load test data

Lithium Battery :6S      22.2V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

Accelerat
Or

21.88

1573

6.44

2555

140.91

11.16

0.53

40%

21.85

1937

8.69

2822

189.88

10.20

0.64

45%

21.82

2403

11.84

3107

258.35

9.30

0.79

50%

21.77

2868

15.43

3377

335.91

8.54

0.95

55%

21.73

3215

18.79

3619

408.31

7.87

1.08

60%

21.69

3579

22.65

3839

491.28

7.29

1.22

65%

21.62

3973

26.94

4053

582.44

6.82

1.37

70%

21.58

4352

31.74

4259

684.95

6.35

1.54

75%

21.52

4789

37.05

4444

797.32

6.01

1.71

80%

21.46

5150

42.44

4637

910.76

5.65

1.88

85%

21.38

5577

48.45

4804

1035.86

5.38

2.06

90%

21.2g

5996

55.2

4931

1175.21

5.10

2.28

95%

21.24

6360

61.63

5017

1309.02

4.86

2.49

100%

Load test data

Lithium Battery:6S  24V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

Accelerat
Or

23.66

1761

7.15

2699

169.17

10.41

0.60

   40%

23.66

2146

9.55

3001

225.95

9.50

0.72

   45%

23.59

2631

13.0

3303

306.91

8.57

0.89

   50%

23.54

3126

16.82

3569

395.94

7.90

1.06

   55%

23.52

3514

20.6

3815

484.51

7.25

1.21

   60%

23.44

3975

25.08

4026

587.88

6.76

1.39

   65%

23.42

4406

29.83

4236

698.62

6.31

1.58

   70%

23.33

4832

34.79

4444

811.65

5.95

1.74

   75%

23.28

5349

40.69

4613

947.26

5.65

1.9

   80%

23.21

5715

46.75

4783

1085.07

5.27

2.17

   85%

23.12

6048

53.16

4922

1229.06

4.92

2.38

   90%

23.05

6461

59.32

5064

1367.33

4.73

2.58

   95%

22.98

6762

65.54

5184

1506.11

4.49

2.77

  100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM6510 KV360

60A
(4S-6S)

P1865
18 inch 

Multi-rotor
drone

1.6KG-2.2KG
uniaxial

5.2KG

1054W

Load test data

Lithium Battery :6S     22.2V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

Accelerat
Or

21.91

930

3.74

2994

81.94

11.35

0.26

40%

21.89

1164

5.08

3370

111.20

10.47

0.32

45%

21.88

1421

6.81

3741

149.00

9.54

0.38

50%

21.83

1695

8.61

4080

187.96

9.02

0.44

55%

21.83

1954

10.72

4401

234.02

8.35

0.51

60%

21.77

2191

12.87

4705

280.18

7.82

0.57

65%

21.76

2516

15.58

4994

339.02

7.42

0.65

70%

21.73

2869

19.02

5316

413.30

6.94

0.74

75%

21.69

3239

22.8

5629

494.53

6.55

0.84

80%

21.63

3619

26.76

5930

578.82

6.25

0.93

85%

21.59

3950

31.13

6228

672.10

5.88

1.03

90%

21.52

4304

35.76

6496

769.56

5.59

1.13

95%

21.44

4674

40.69

6754

872.39

5.36

1.23

100%

Load test data

Lithium Battery :6S        24V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

Accelerat
Or

23.71

1017

4.16

3225

98.63

10.31

0.29

40%

23.68

1303

5.76

3641

136.40

9.55

0.36

45%

23.67

1588

7.65

4023

181.08

8.77

0.43

50%

23.62

1903

9.75

4372

230.30

8.26

0.50

55%

23.60

2262

12.39

4693

292.40

7.74

0.60

60%

23.57

2540

14.65

4989

345.30

7.36

0.66

65%

23.54

2909

18.09

5326

425.84

6.83

0.76

70%

23.51

3268

21.64

5670

508.76

6.42

0.86

75%

23.46

3641

25.45

5989

597.06

6.10

0.95

80%

23.39

4027

30.05

6315

702.87

5.73

1.06

85%

23.33

4447

34.86

6614

813.28

5.47

1.17

90%

23.29

4836

39.85

6891

928.11

5.21

1.29

95%

23.22

5248

45.41

7153

1054.42

4.98

1.41

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM6510 KV360

60A
(4S-6S)

P2070
20 inch 

Multi-rotor
drone

2.2KG-2.8KG
uniaxial  

6.4KG

1394W

Load test data

Lithium Battery :6S      22.2V

Voltage(V)

Pulling
Force(g)

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

Accelerat
Or

   21.88

1268

5.22

2839

114.21

11.10

0.38

40%

   21.85

1588

7.22

3196

157.76

10.07

0.47

45%

   21.84

1961

9.85

3558

215.12

9.12

0.58

50%

  21.79

2308

12.57

3858

273.90

8.43

0.68

55%

   21.77

2660

15.49

4139

337.22

7.89

0.78

60%

   21.73

3032

18.99

4408

412.65

7.35

0.89

65%

   21.68

3420

22.92

4673

496.91

6.88

1.02

70%

   21.63

3827

27.21

4931

588.55

6.50

1.14

75%

   21.57

4256

32.13

5184

693.04

6.14

1.28

80%

   21.49

4674

37.73

5427

810.82

5.76

1.43

85%

   21.44

5085

43.39

5664

930.28

5.47

1.57

90%

   21.38

5456

48.97

5885

1046.98

5.21

1.70

95%

   21.2g

5877

55.21

6075

1175.42

5.00

1.85

100%

Load test data

Lithium Battery :6S        24V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficiency

(g/W）

Torque
(N.m)

accelerat
Or

23.68

1451

5.87

3032

139.00

10.44

0.44

40%

23.66

1836

8.34

3430

197.32

9.30

0.55

45%

23.62

2227

11.11

3791

262.42

8.49

0.66

50%

23.59

2584

14.01

4114

330.50

7.82

0.77

55%

23.55

3027

17.54

4393

413.07

7.33

0.90

60%

23.53

3483

21.53

4660

506.60

6.88

1.04

65%

23.45

3848

25.34

4944

594.22

6.48

1.15

70%

23.38

4290

30.36

5219

709.82

6.04

1.30

75%

23.33

4734

35.71

5482

833.11

5.68

1.45

80%

23.28

5181

41.37

5730

963.09

5.38

1.61

85%

23.20

5569

47.65

5975

1105.48

5.04

1.77

90%

23.13

6015

54.07

6186

1250.64

4.81

1.93

95%

23.03

6441

60.55

6389

1394.47

4.62

2.08

100%