FY70-8311 Brushless Long Shaft high-power Brushless Motor Electric Fixed Wing Aircraft VTOL UAV

Power configuration Measured data

Motor

ESC

propeller

Applicable

models

Applicable

Takeoff weight

Max thrust

Max power

FY70 KV120

80A

(6S-14S)

P2680

26 inch straight

propeller

multi-rotor

drone

4.0KG-5.0KG

uniaxial

(Single axis)

10.2KG

2042W

load test data

Lithium Battery :12S     44.4V

Voltage(V)

Thrust(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W)

Torque

(N.m)

accelerator

44.17

1873

3.24

1931

143.11

13.09

0.71

40%

44.13

2409

4.63

2191

204.32

11.79

0.89

45%

44.13

2955

6.23

2424

274.93

10.75

1.08

50%

44.11

3448

7.77

2608

342.73

10.06

1.26

55%

44.07

4028

9.77

2816

430.56

9.36

1.46

60%

44.07

4664

12.21

3024

538.09

8.67

1.70

65%

44.02

5223

14.48

3205

637.41

8.19

1.90

70%

43.98

5940

17.65

3421

776.25

7.65

2.17

75%

43.96

6613

21.15

3607

929.75

7.11

2.46

80%

43.92

7316

24.94

3794

1095.36

6.68

2.76

85%

43.86

7948

28.97

3960

1270.62

6.26

3.06

90%

43.81

8598

33.21

4124

1454.93

5.91

3.37

95%

43.74

9304

38.07

4271

1665.18

5.59

3.72

100%

load test data

Lithium Battery :12S       48V

Voltage(V)

Thrust

(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W)

Torque

(N.m)

accelerator

47.75

2194

3.83

2086

182.88

12.00

0.84

40%

47.76

2779

5.41

2353

258.38

10.76

1.05

45%

47.72

3395

7.25

2594

345.97

9.81

1.27

50%

47.71

4011

8.96

2787

427.48

9.38

1.46

55%

47.68

4640

11.33

3006

540.21

8.59

1.72

60%

47.64

5307

13.84

3205

659.34

8.05

1.96

65%

47.57

6041

16.82

3418

800.13

7.55

2.24

70%

47.55

6752

20.34

3616

967.17

6.98

2.55

75%

47.54

7392

24.24

3824

1152.37

6.41

2.88

80%

47.49

8042

28.05

3997

1332.09

6.04

3.18

85%

47.43

8781

32.67

4187

1549.54

5.67

3.53

90%

47.36

9458

37.35

4339

1768.90

5.35

3.89

95%

47.29

10218

43.19

4475

2042.46

5.00

4.36

100%

Power configuration Measured data

Motor

ESC

propeller

Applicable

models

Applicable

Takeoff weight

Max thrust

Max power

FY70 KV120

80A

(6S-14S)

P2880

28 inch straight propeller

multi-roto

drone

4.0KG-5.0KG

Uniaxia

(Single axis)

10.9KG

2471W

load test data

Lithium Battery:12S      44.4V

Voltage(V)

Thrust

(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W)

Torque

(N.m)

accelerator

44.13

2311

4.27

1874

188.44

12.26

  0.96

40%

44.12

2914

6.05

2125

266.93

10.92

  1.20

45%

44.08

3557

7.87

2342

346.91

10.25

  1.41

50%

44.07

4324

10.59

2556

466.70

9.27

  1.74

55%

44.06

4836

12.68

2714

558.68

8.66

  1.97

60%

43.99

5504

15.6

2915

686.24

8.02

  2.25

65%

43.98

6308

19.04

3099

837.38

7.53

  2.58

70%

43.94

6799

22.28

3261

978.98

6.94

  2.87

75%

43.88

7796

26.95

3433

1182.57

6.59

  3.29

80%

43.84

8627

32.07

3585

1405.95

6.14

  3.75

85%

43.75

9027

36.72

3733

1606.50

5.62

  4.11

90%

43.71

9804

41.83

3858

1828.39

5.36

  4.53

95%

43.64

10373

47.32

3955

2065.04

5.02

  4.99

100%

load test data

Lithium Battery :12S 48V

Voltage(V)

Thrust

(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W)

Torque

(N.m)

accelerator

47.74

2677

4.84

2024

231.06

11.59

1.09

40%

47.71

3369

6.77

2273

323.00

10.43

1.36

45%

47.66

4124

9.16

2503

436.57

9.45

1.67

50%

47.66

4766

11.38

2682

542.37

8.79

1.93

55%

47.62

5499

14.38

2890

684.78

8.03

2.26

60%

47.59

6290

17.7

3086

842.34

7.47

2.61

65%

47.57

7142

21.48

3254

1021.80

6.99

3.00

70%

47.51

7891

25.57

3429

1214.83

6.50

3.38

75%

47.44

8650

30.36

3581

1440.28

6.01

3.84

80%

47.37

9318

35.56

3738

1684.48

5.53

4.30

85%

47.31

9974

41.23

3863

1950.59

5.11

4.82

90%

47.26

10551

46.44

3960

2194.75

4.81

5.29

95%

47.18

10923

52.39

4013

2471.76

4.42

5.88

100%

Power configuration Measured data

Motor

ESC

propeller

Applicable

models

Applicable

Takeoff weight

Max thrust

Max power

FY70 KV120

80A

(6S-14S)

P3095

30 inch straight

propeller

multi-rotor

drone

4.2KG-5.2KG

uniaxial

(Single axis)

11.1KG

2641W

load test data

Lithium Battery:12S      44.4V

Voltage(V)

Thrust

(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W)

Torque

(N.m)

accelerator

44.12

2626

4.69

1843

206.92

12.69

  1.07

40%

44.09

3308

6.66

2079

293.64

11.27

  1.35

45%

44.07

4052

8.88

2294

391.34

10.35

  1.63

50%

44.06

4931

11.95

2484

526.52

9.37

  2.02

55%

44.05

5512

14.19

2642

625.07

8.82

  2.26

60%

43.97

6341

17.6

2830

773.87

8.19

  2.61

65%

43.94

7097

21.16

3003

929.77

7.63

  2.96

70%

43.92

7835

25.15

3158

1104.59

7.09

  3.34

75%

43.82

8579

29.94

3330

1311.97

6.54

  3.76

80%

43.79

9281

34.99

3461

1532.21

6.06

  4.23

85%

43.72

10034

40.54

3573

1772.41

5.66

  4.74

90%

43.68

10461

45.43

3678

1984.38

5.27

  5.15

95%

43.58

11053

51.57

3747

2247.42

4.92

  5.73

100%

load test data

Lithium Battery :12S       48V

Voltage(V)

Thrust

(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W)

Torque

(N.m)

accelerator

47.76

3054

5.46

1967

260.77

11.71

1.27

   40%

47.71

3791

7.63

2217

364.03

10.41

1.57

   45%

47.71

4662

10.29

2430

490.94

9.50

1.93

   50%

47.65

5380

12.59

2605

599.91

8.97

2.20

   55%

47.62

6283

16.13

2800

768.11

8.18

2.62

   60%

47.57

7046

19.59

2976

931.90

7.56

2.99

   65%

47.53

7757

23.14

3128

1099.84

7.05

3.36

   70%

47.48

8550

28.26

3304

1341.78

6.37

3.88

   75%

47.41

9333

33.28

3449

1577.80

5.92

4.37

   80%

47.35

9927

38.84

3564

1839.07

5.40

4.93

   85%

47.25

10492

44.25

3669

2090.81

5.02

5.44

   90%

47.23

10917

50.29

3738

2375.20

4.60

6.07

   95%

47.12

11221

56.06

3794

2641.55

4.25

6.65

  100%

Power configuration Measured data

Motor

ESC

propeller

Applicable

models

Applicable

Takeoff weight

Max thrust

Max power

FY70 KV140

80A

(6S-14S)

P2480

24 inch straight

propeller

multi-rotor

drone

3.5KG-4.8KG

uniaxia

(Single axis)

11KG

2420W

load test data

Lithium Battery:12S      44.4V

Voltage(V)

Thrust

(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W)

Torque

(N.m)

accelerator

44.16

1993

4.29

0.579

189.45

10.52

3124.72

40%

44.13

2466

5.53

0.713

244.04

10.10

3268.68

45%

44.11

3005

7.43

0.865

327.74

9.17

3618.37

50%

44.09

3471

9.24

1.001

407.39

8.52

3886.70

55%

44.03

4082

11.46

1.176

504.58

8.09

4097.60

60%

43.98

4809

14.47

1.389

636.39

7.56

4375.47

65%

43.95

5482

18.04

1.575

792.86

6.91

4807.49

70%

43.93

6083

20.93

1.762

919.45

6.62

4983.42

75%

43.92

6859

25.09

1.984

1101.95

6.22

5304.26

80%

43.86

7614

29.61

2.212

1298.69

5.86

5606.93

85%

43.79

8407

34.51

2.448

1511.19

5.56

5895.38

90%

43.74

8945

39.15

2.627

1712.42

5.22

6225.21

95%

43.66

9623

44.56

2.834

1945.49

4.95

6555.90

100%

load test data

Lithium Battery :12S       48V

Voltage(V)

Thrust

(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W)

Torque

(N.m)

accelerator

47.74

2308

4.78

2563

228.20

10.11

0.85

40%

47.74

2878

6.41

2827

306.01

9.40

1.03

45%

47.71

3495

8.51

3118

406.0

8.61

1.24

50%

47.68

4081

10.63

3360

506.84

8.05

1.44

55%

47.64

4697

13.09

3629

623.61

7.53

1.64

60%

47.62

5497

16.48

3898

784.78

7.00

1.92

65%

47.57

6179

19.64

4112

934.27

6.61

2.17

70%

47.52

6984

23.62

4371

1122.42

6.22

2.45

75%

47.47

7829

28.23

4606

1340.08

5.84

2.78

80%

47.42

8723

33.19

4837

1573.87

5.54

3.11

85%

47.33

9387

38.25

5057

1810.37

5.19

3.42

90%

47.25

10148

43.94

5243

2076.17

4.89

3.78

95%

47.21

11064

51.27

5424

2420.46

4.57

4.26

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable

models

Applicable

Takeoff weight

Max thrust

Max power

FY70 KV140

80A

(6S-14S)

P2680

26 inch straight

propeller

multi-rotor

drone

4.0KG-5.0KG

uniaxia

(Single axis)

11.9KG

3085W

load test data

Lithium Battery:12S      44.4V

Voltage(V)

Thrust

(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W)

Torque

(N.m)

accelerator

44.16

2197

3.89

2086

171.78

12.79

0.79

40%

44.13

2778

5.39

2353

237.86

11.68

0.97

45%

44.11

3398

7.09

2590

312.74

10.87

1.15

50%

44.09

3983

8.99

2790

396.37

10.05

1.36

55%

44.03

4620

11.2

3006

493.14

9.37

1.57

60%

43.98

5295

13.97

3209

614.40

8.62

1.83

65%

43.95

6044

16.9

3418

742.76

8.14

2.08

70%

43.93

6742

20.38

3611

895.29

7.53

2.37

75%

43.92

7384

24.24

3824

1064.62

6.94

2.66

80%

43.86

8059

28.01

3997

1228.52

6.56

2.94

85%

43.79

8891

32.89

4181

1440.25

6.17

3.29

90%

43.74

9508

37.46

4339

1638.50

5.80

3.61

95%

43.66

10250

43.22

4482

1886.99

5.43

4.02

100%

load test data

Lithium Battery:12S        48V

Voltage(V)

Thrust

(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W)

Torque

(N.m)

accelerator

47.72

3106

6.37

2478

303.98

10.22

1.17

40%

47.71

3783

8.48

2726

404.58

9.35

1.42

45%

47.66

4481

11.08

2997

528.07

8.49

1.68

50%

47.63

5295

14.11

3236

672.06

7.88

1.98

55%

47.59

6016

17.66

3481

840.44

7.16

2.31

60%

47.53

6872

21.74

3714

1033.30

6.65

2.66

65%

47.48

7766

26.56

3919

1261.07

6.16

3.07

70%

47.41

8676

31.63

4118

1499.58

5.79

3.48

75%

47.37

9479

37.32

4320

1767.85

5.36

3.91

80%

47.28

10304

43.99

4495

2079.85

4.95

4.42

85%

47.18

10970

51.11

4642

2411.37

4.55

4.96

90%

47.11

11565

57.95

4752

2730.02

4.24

5.49

95%

47.02

11963

65.63

4813

3085.92

3.88

6.12

100%

Power configuration Measured data

Motor

ESC

propeller

Applicable

models

Applicable

Takeoff weight

Max thrust

Max power

FY70 KV160

80A

(6S-14S)

P2280

22 inch straight

propeller

multi-rotor

drone

3.5KG-4.5KG

uniaxial

(Single axis)

10.6KG

2445W

load test data

Lithium Battery:12S      44.4V

Voltage(V)

Thrust

(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W)

Torque

(N.m)

accelerator

44.11

1962

4.34

2697

191.44

10.25

0.68

40%

44.13

2439

5.89

3000

259.93

9.38

0.83

45%

44.11

2917

7.61

3283

335.68

8.69

0.98

50%

44.08

3474

9.71

3568

428.02

8.12

1.15

55%

44.05

4103

12.22

3863

538.29

7.62

1.33

60%

44.03

4645

14.55

4096

640.64

7.25

1.49

65%

43.99

5252

17.9

4396

787.42

6.67

1.71

70%

43.95

5902

21.53

4671

946.24

6.24

1.93

75%

43.88

6534

25.58

4949

1122.45

5.82

2.17

80%

43.84

7452

30.44

5207

1334.49

5.58

2.45

85%

43.78

8086

35.02

5444

1533.18

5.27

2.69

90%

43.72

8841

39.97

5660

1747.49

5.06

2.95

95%

43.69

9626

46.23

5882

2019.79

4.77

3.28

100%

load test data

Lithium Battery:12S        48V

Voltage(V)

Thrust

(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W)

Torque

(N.m)

accelerator

47.76

2233

4.84

2890

231.16

9.66

0.76

40%

47.74

2703

6.36

3198

303.63

8.90

0.91

45%

47.71

3336

8.39

3506

400.29

8.33

1.09

50%

47.69

3990

10.98

3833

523.64

7.62

1.30

55%

47.65

4441

12.98

4057

618.50

7.18

1.46

60%

47.61

5087

16.01

4383

762.24

6.67

1.66

65%

47.58

5653

19.23

4700

914.96

6.18

1.86

70%

47.52

6561

23.61

4982

1121.95

5.85

2.15

75%

47.48

7330

28.01

5253

1329.91

5.51

2.42

80%

47.43

8095

32.84

5534

1557.60

5.20

2.69

85%

47.35

8836

38.32

5791

1814.45

4.87

2.99

90%

47.27

9709

44.45

5988

2101.15

4.62

3.35

95%

47.21

10685

51.79

6199

2445.01

4.37

3.77

100%

Power configuration Measured data

Motor

ESC

propeller

Applicable

models

Applicable

Takeoff weight

Max thrust

Max power

FY70 KV160

80A

(6S-14S)

F2360

23 inch straight

propeller

multi-rotor

drone

3.5KG-4.5KG

uniaxial

(Single axis)

10.3KG

2239W

load test data

Lithium Battery :12S     44.4V

Voltage(V)

Thrust

(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W)

Torque

(N.m)

accelerator

44.15

1844

3.98

2709

175.72

10.49

0.62

40%

44.13

2363

5.44

3015

240.07

9.84

0.76

45%

44.11

2766

6.81

3304

300.39

9.21

0.87

50%

44.11

3184

8.59

3607

378.90

8.40

1.00

55%

44.08

3707

10.14

3903

446.97

8.29

1.09

60%

44.04

4289

12.98

4147

571.64

7.50

1.32

65%

43.99

4997

16.11

4462

708.68

7.05

1.52

70%

43.97

5676

19.45

4730

855.22

6.64

1.73

75%

43.94

6515

23.65

5015

1039.18

6.27

1.98

80%

43.83

7083

27.77

5271

1217.16

5.82

2.21

85%

43.82

7771

32.22

5544

1411.88

5.50

2.43

90%

43.77

8374

36.67

5769

1605.05

5.22

2.66

95%

43.69

9239

42.18

6012

1842.84

5.01

2.93

100%

load test data

Lithium Battery :12S       48V

Voltage(V)

Thrust

(g)

Current(A)

RPM

Power(W)

Efficien

cy(g/W)

Torque

(N.m)

accelerator

47.75

2123

4.54

2907

216.79

9.79

0.71

40%

47.73

2626

6.03

3219

287.81

9.12

0.85

45%

47.73

3183

7.92

3535

378.02

8.42

1.02

50%

47.67

3802

10.45

3863

498.15

7.63

1.23

55%

47.65

4277

12.02

4101

572.75

7.47

1.33

60%

47.63

5046

15.34

4422

730.64

6.91

1.58

65%

47.59

5713

18.63

4722

886.60

6.44

1.79

70%

47.52

6402

22.55

5032

1071.58

5.97

2.03

75%

47.48

7151

26.53

5318

1259.64

5.68

2.26

80%

47.39

8036

31.33

5596

1484.73

5.41

2.53

85%

47.38

8819

36.43

5859

1726.05

5.11

2.81

90%

47.34

9497

41.15

6098

1948.04

4.88

3.05

95%

47.24

10314

47.41

6343

2239.65

4.61

3.37

100%