FY90-8017 fast speed powerful electric UAV motor electric brushless DC bldc drone motor

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max  thrust

Max power

FY90 KV105

80A
(6S-14S)

P2880
28 inch straight
propeller

Multi-rotor
drone

5.5KG-7.0KG
uniaxial

16.4KG

3606W

Load test data

Lithium Battery:14S 51.8V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

51.56

2930

4.76

1388

245.43

11.94

1.69

40%

51.51

3663

6.51

1547

335.33

10.92

2.07

45%

51.51

4706

9.17

1727

472.35

9.96

2.61

50%

51.45

5642

11.84

1896

609.17

9.26

3.07

55%

51.42

6472

14.89

2041

765.64

8.45

3.58

60%

51.39

7395

18.26

2178

938.38

7.88

4.11

65%

51.35

8300

22.18

2314

1138.94

7.29

4.70

70%

51.31

9205

27.07

2458

1388.96

6.63

5.40

75%

51.25

10115

31.49

2585

1613.86

6.27

5.96

80%

51.19

11287

36.95

2723

1891.47

5.97

6.63

85%

51.11

12420

43.66

2845

2231.46

5.57

7.49

90%

50.99

13600

50.48

2961

2573.98

5.28

8.30

95%

50.91

14834

58.23

3069

2964.49

5.00

9.22

100%

Load test data

Lithium Battery:14S        56V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

55.72

3350

5.44

1481

303.12

  11.05

1.95

   40%

55.71

4254

7.54

1664

420.05

  10.13

2.41

   45%

55.71

5313

10.44

1858

581.61

  9.13

2.99

   50%

55.68

6316

13.56

2028

755.02

  8.37

3.56

   55%

55.61

7288

16.82

2175

935.36

  7.79

4.11

   60%

55.57

8102

20.72

2320

1151.41

  7.04

4.74

   65%

55.53

9332

25.49

2462

1415.46

  6.59

5.49

   70%

55.47

10280

30.04

2597

1666.32

  6.17

6.13

   75%

55.41

11549

35.72

2741

1979.25

  5.84

6.90

   80%

55.35

12825

42.08

2877

2329.13

  5.51

7.73

   85%

55.25

13977

48.95

3004

2704.49

  5.17

8.60

   90%

55.16

15094

55.95

3116

3086.20

  4.89

9.46

   95%

55.05

16416

65.51

3247

3606.33

  4.55

10.61

  100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max  thrust

Max power

FY90 KV105

80A
(6S-14S)

P3095
30 inch straight
propeller

Multi-rotor
drone

5.0KG-6.5KG
uniaxial

14.7KG

2655W

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

2653

4.43

1203

195.67

13.56

1.55

40%

44.14

3186

5.99

1328

264.40

12.05

1.90

45%

44.11

3974

7.85

1473

346.26

11.48

2.24

50%

44.08

4827

10.43

1623

459.75

10.50

2.71

55%

44.05

5778

13.57

1759

597.76

9.67

3.25

60%

43.99

6606

16.46

1876

724.08

9.12

3.69

65%

43.98

7277

19.48

1999

856.73

8.49

4.09

70%

43.93

8249

23.41

2121

1028.40

8.02

4.63

75%

43.86

9106

27.62

2245

1211.41

7.52

5.15

80%

43.82

10080

32.37

2366

1418.45

7.11

5.73

85%

43.73

11104

38.23

2477

1671.80

6.64

6.45

90%

43.71

12146

43.72

2583

1911.00

6.36

7.07

95%

43.63

13054

49.65

2695

2166.23

6.03

7.68

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

2991

4.98

1284

237.84

12.58

1.77

40%

47.75

3627

6.62

1422

316.11

11.47

2.12

45%

47.71

4675

9.13

1582

435.59

10.73

2.63

50%

47.69

5527

11.9

1747

567.51

9.74

3.10

55%

47.63

6390

14.94

1886

711.59

8.98

3.60

60%

47.59

7267

18.22

2013

867.09

8.38

4.11

65%

47.55

8082

21.55

2142

1024.70

7.89

4.57

70%

47.52

9205

26.6

2265

1264.03

7.28

5.33

75%

47.46

10101

30.98

2394

1470.31

6.87

5.87

80%

47.36

11273

36.84

2514

1744.74

6.46

6.63

85%

47.32

12421

42.66

2640

2018.67

6.15

7.30

90%

47.23

13604

49.28

274

2327.49

5.84

8.11

95%

47.14

14711

56.34

2843

2655.87

5.54

8.92

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max  thrust

Max power

FY90 KV105

80A
(6S-14S)

P3210
32 inch straight
propeller

Multi-rotor
drone

5.5KG-7.0KG
uniaxia

15KG

2737W

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

3333

5.75

1174

253.75

13.14

2.06

40%

44.11

4088

7.65

1296

337.44

12.11

2.49

45%

44.10

4929

10.15

1427

447.62

11.01

3.00

50%

44.05

5917

13.16

1568

579.70

10.21

3.53

55%

43.99

6957

17.01

1698

748.27

9.30

4.21

60%

43.95

7878

20.83

1817

915.48

8.61

4.81

65%

43.92

8808

24.87

1916

1092.29

8.06

5.44

70%

43.82

9948

30.17

2031

1322.05

7.52

6.22

75%

43.77

11126

35.67

2132

1561.28

7.13

6.99

80%

43.71

12085

41.89

2238

1831.01

6.60

7.81

85%

43.64

13158

48.88

2339

2133.12

6.17

8.71

90%

43.54

14111

55.99

2433

2437.80

5.79

9.57

95%

43.43

15045

63.03

2523

2737.39

5.50

10.36

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

47.73

3798

6.33

1250

302.13

12.57

2.31

40%

47.73

4622

8.51

1380

406.18

11.38

2.81

45%

47.64

5698

11.54

1526

549.77

10.36

3.44

50%

47.61

6748

15.08

1678

717.96

9.40

4.09

55%

47.58

7907

19.12

1810

909.73

869

4.80

60%

47.53

8887

23.14

1925

1099.84

8.08

5.46

65%

47.47

10064

28.02

2036

1330.11

7.57

6.24

70%

47.39

11260

33.64

2144

1594.20

7.06

7.10

75%

47.32

12432

39.7

2261

1878.60

6.62

7.93

80%

47.26

13584

46.75

2364

2209.41

6.15

8.93

85%

47.14

14678

54.26

2462

2557.82

5.74

9.92

90%

47.07

15890

62.46

2548

2939.99

5.40

11.02

95%

46.95

17195

71.71

2630

3366.78

5.11

12.23

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max  thrust

Max power

FY90 KV125

80A
(6S-14S)

P2880
28 inch straight
propeller

Multi-rotor
drone

5.0KG-6.5KG
uniaxial

15,3KG

3210W

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

2642

5.14

1325

226.98

11.64

  1.64

40%

44.12

3294

6.87

1475

303.10

10.87

  1.96

45%

44.10

4163

9.45

1647

416.75

9.99

  2.42

50%

44.07

5102

12.53

1812

552.20

9.24

  2.91

55%

44.04

5931

15.7

1947

691.43

8.58

  3.39

60%

43.98

6837

19.09

2087

839.58

8.14

  3.84

65%

43.92

7581

22.94

2217

1007.52

7.52

  4.34

70%

43.88

8479

27.81

2350

1220.30

6.95

  4.96

75%

43.80

9374

33.22

2481

1455.04

6.44

  5.60

80%

43.72

10404

38.78

2613

1695.46

6.14

  6.20

85%

43.67

11489

45.68

2731

1994.85

5.76

  6.98

90%

43.57

12589

52.85

2845

2302.67

5.47

  7.73

95%

43.46

13451

60.34

2952

2622.38

5.13

  8.48

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

2994

5.63

1426

268.78

11.14

1.80

40%

47.72

3861

7.99

1595

381.28

10.13

2.28

45%

47.67

4656

10.78

1785

513.88

9.06

2.75

50%

47.64

5669

14.11

1946

672.20

8.43

3.30

55%

47.61

6590

17.55

2095

835.56

7.89

3.81

60%

47.55

7493

21.93

2226

1042.77

7.19

4.47

65%

47.48

8384

26.21

2370

1244.45

6.74

5.01

70%

47.45

9429

31.55

2490

1497.05

6.30

5.74

75%

47.37

10623

37.94

2628

1797.22

5.91

6.53

80%

47.26

11995

44.31

2763

2094.09

5.73

7.24

85%

47.21

13001

51.56

2892

2434.15

5.34

8.04

90%

47.08

14020

59.73

3001

2812.09

4.99

8.95

95%

46.99

15389

68.33

3102

3210.83

4.79

9.89

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max  thrust

Max power

FY90 KV125

80A
6S-14S)

P3095
30 inch straight
propeller

Multi-rotor
drone

5.5KG-7.5KG
uniaxial

16,3KG

3422W

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

44.14

3166

5.83

1326

257.34

12.30

1.85

40%

44.11

3898

7.9

1475

348.47

11.19

2.26

45%

44.09

4962

10.9

1638

480.58

10.33

2.80

50%

44.04

5853

14.25

1801

627.57

9.33

3.33

55%

44.01

6716

17.55

1933

772.38

8.70

3.82

60%

43.92

7758

21.6

2063

948.67

8.18

4.39

65%

43.89

8537

25.39

2191

1114.37

7.66

4.86

70%

43.84

9634

31.03

2322

1360.36

7.08

5.59

75%

43.78

10762

36.85

2445

1613.29

6.67

6.30

80%

43.68

11795

43.3

2559

1891.34

6.24

7.06

85%

43.62

12864

50.51

2675

2203.25

5.84

7.87

90%

43.50

14039

57.34

2787

2494.29

5.63

8.55

95%

43.42

15022

65.18

2889

2830.12

5.31

9.36

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

3616

6.64

1410

316.99

  11.4

  2.15

40%

47.72

4514

9.06

1578

432.34

  10.44

  2.62

45%

47.63

5562

12.19

1758

580.61

  9.58

  3.15

50%

47.62

6646

15.96

1916

760.02

  8.74

  3.79

55%

47.56

7682

19.84

2053

943.59

  8.14

  4.39

60%

47.49

8573

24.25

2188

1151.63

  7.44

  5.03

65%

47.46

9642

29.28

2322

1389.63

  6.94

  5.72

70%

47.39

10789

34.58

2460

1638.75

  6.58

  6.36

75%

47.33

11779

40.92

2580

1936.74

  6.08

  7.17

80%

47.22

13332

48.58

2697

2293.95

  5.81

  8.12

85%

47.16

14505

56.07

2817

2644.26

  5.49

  8.96

90%

47.05

15708

64.59

2924

3038.96

  5.17

  9.93

95%

46.94

16365

72.92

3030

3422.86

4.78

10.79

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max  thrust

Max power

FY90 KV125

120A
(6S-14S

P3210
32 inch straight
propeller

Multi-rotor
drone

6.0KG-8.0KG
uniaxia

18.6KG

4266W

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

4064

7.63

1292

336.64

12.07

2.49

40%

44.09

4918

10.18

1427

448.84

10.96

3.00

45%

44.05

5942

13.65

1582

601.28

9.88

3.63

50%

43.97

7282

18.15

1727

798.06

9.12

4.41

55%

43.92

8440

22.94

1861

1007.52

8.38

5.17

60%

43.88

9427

27.33

1976

1199.24

7.86

5.80

65%

43.82

10732

33.15

2083

1452.63

7.39

6.66

70%

43.74

11756

39.26

2193

1717.23

6.85

7.48

75%

43.66

12661

45.8

2309

1999.63

6.33

8.27

80%

43.57

14084

54.63

2400

2380.23

5.92

9.47

85%

43.47

14934

62.68

2501

2724.70

5.48

10.40

90%

43.35

16220

71.96

2585

3119.47

5.20

11.52

95%

43.24

17104

81.22

2660

3511.95

4.87

12.61

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

   47.73

4525

8.38

1369

399.98

11.31

  2.79

40%

   47.67

5638

11.44

1517

545.34

10.34

  3.43

45%

   47.63

6865

15.13

1685

720.64

9.53

  4.08

50%

   47.59

8034

19.85

1840

944.66

8.50

  4.90

55%

   47.48

9489

25.07

1958

1190.32

7.97

  5.81

60%

   47.45

10665

30.97

2079

1469.53

7.26

  6.75

65%

   47.38

11918

37.07

2191

1756.38

6.79

  7.66

70%

   47.30

12998

43.81

2312

2072.21

6.27

  8.56

75%

   47.18

14293

52.21

2412

2463.27

5.80

  9.75

80%

   47.09

15342

60.2

2512

2834.82

5.41

 10.78

85%

   46.97

16439

69.24

2611

3252.20

5.05

 11.90

90%

   46.87

17696

79.31

2695

3717.26

4.76

 13.17

95%

   46.75

18673

91.27

2757

4266.87

4.38

 14.78

100%HOT

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max  thrust

Max power

FY90 KV180

120A
(6S-14S)

P2480
24 inch straight
propeller

Multi-rotor
drone

6.0KG-8.0KG
uniaxial

17.1KG

4645W

Load test data

Lithium Battery :12S     44.4V

Voltage(V)

Pulling
Force(g)

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

44.09

3215

8.71

2978

384.02

8.37

1.23

40%

44.04

4028

11.73

3339

516.59

7.80

1.48

45%

44.01

4787

15.13

3668

665.87

7.19

1.73

50%

43.98

5695

19.03

3935

836.94

6.80

2.03

55%

43.92

6264

23.13

4222

1015.87

6.17

2.30

60%

43.87

7364

28.62

4493

1255.56

5.87

2.67

65%

43.78

8321

34.56

4800

1513.04

5.50

3.01

70%

43.71

9087

40.48

5110

1769.38

5.14

3.31

75%

43.59

10334

48.6

5366

2118.47

4.88

3.77

80%

43.51

11733

57.88

5606

2518.36

4.66

4.29

85%

43.39

12929

68.04

5851

2952.26

4.38

4.82

90%

43.28

13861

77.13

6084

3338.19

4.15

5.24

95%

43.13

15132

88.32

6290

3809.24

3.97

5.78

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

47.69

3809

9.98

3220

475.95

  8.00

1.41

40%

47.62

4662

13.44

3591

640.01

  7.28

1.70

45%

47.59

5455

16.95

3881

806.65

  6.76

1.98

50%

47.55

6341

21.61

4205

1027.56

  6.17

2.33

55%

47.48

7394

26.42

4488

1254.42

  5.89

2.67

60%

47.41

8602

32.5

4800

1540.83

  5.58

3.07

65%

47.34

9678

39.54

5104

1871.82

  5.17

3.50

70%

47.26

10844

47.67

5394

2252.88

  4.81

3.99

75%

47.14

12293

56.33

5658

2655.40

  4.63

4.48

80%

47.03

13563

66.14

5924

3110.56

  4.36

5.01

85%

46.91

14609

75.59

6190

3545.93

  4.12

5.47

90%

46.77

15914

86.56

6393

4048.41

  3.93

6.05

95%

46.62

17152

99.65

6611

4645.68

  3.69

6.71

100%HOT