FM501(5010) RC Airplane Motor For Strong Power Avion/Drone

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM501 KV200

60A
(4-6S)

F2480
24 inch folding
propeller

Multi-rotor
drone

1.5KG-2.1KG
(One axis)

3.61KG

538W

Load test data

Lithium Battery :6S     22.2V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

22.02

1000

2.9

1605

63.86

15.66

0.38

40%

21.99

1211

3.91

1763

85.98

14.08

0.47

45%

22.01

1405

5.09

1926

112.03

12.54

0.56

50%

21.98

1688

6.35

2071

139.57

12.09

0.64

55%

21.95

1885

7.71

2206

169.23

11.14

0.73

60%

21.96

2139

9.35

2332

205.33

10.42

0.84

65%

21.92

2359

10.87

2449

238.27

9.90

0.93

70%

21.89

2535

12.59

2562

275.60

9.20

1.03

75%

21.87

2825

14.66

2678

320.61

8.81

1.14

80%

21.87

2986

16.41

2766

358.89

8.32

1.24

85%

21.82

3227

18.58

2861

405.42

7.96

1.35

90%

21.81

3338

20.05

2920

437.29

7.63

1.43

95%

21.79

3410

20.78

2955

452.80

7.53

1.46

100%

Load test data

Lithium Battery :6S       24V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

24.00

1139

3.2

1709

76.80

14.83

0.43

40%

23.98

1381

4.39

1882

105.27

13.12

0.53

45%

23.97

1632

5.66

2042

135.67

12.03

0.63

50%

23.92

1886

6.99

2189

167.20

11.28

0.73

55%

23.94

2127

8.54

2325

204.45

10.40

0.84

60%

23.90

2380

10.4

2463

248.56

9.58

0.96

65%

23.92

2594

12.07

2567

288.71

8.98

1.07

70%

23.88

2865

14.04

2681

335.28

8.55

1.19

75%

23.86

3043

15.93

2788

380.09

8.01

1.30

80%

23.84

3244

18.02

2878

429.60

7.55

1.43

85%

23.81

3453

20.33

2968

484.06

7.13

1.56

90%

23.80

3581

22.12

3010

526.46

6.80

1.67

95%

23.79

3615

22.62

3050

538.13

6.72

1.68

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM501 KV200

60A
4-6S

F2280
22 inch folding
propeller

Multi-rotor,drone

1.4KG-2.0KG/shaft

3.38KG

554W

Load test data

Lithium Battery :6S     22.2V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

22.01

955

3.02

1593

66.47

14.37

0.40

40%

21.99

1153

3.95

1744

86.86

13.27

0.48

45%

21.96

1380

5.08

1903

111.56

12.37

0.56

50%

21.95

1594

6.47

2044

142.02

11.22

0.66

55%

21.96

1817

7.99

2179

175.46

10.36

0.77

60%

21.95

2033

9.62

2302

211.16

9.63

0.88

65%

21.95

2225

11.23

2412

246.50

9.03

0.98

70%

21.92

2432

13.02

2523

285.40

8.52

1.08

75%

21.89

2647

15.01

2632

328.57

8.06

1.19

80%

21.84

2817

16.9

2719

369.10

7.63

1.30

85%

21.84

3025

19.19

2810

419.11

7.22

1.42

90%

21.82

3137

21.05

2855

459.31

6.83

1.54

95%

21.81

3185

21.79

2888

475.24

6.70

1.57

100%

Load test data

Lithium Battery :6S      24V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W）

Torque
(N.m)

Accelerator

24.01

1092

3.54

1697

85.00

12.85

  0.48

40%

23.96

1328

4.63

1868

110.93

11.97

  0.57

45%

23.98

1554

6.03

2025

144.60

10.75

  0.68

50%

23.95

1791

7.51

2169

179.86

9.96

  0.79

55%

23.92

2019

9.08

2302

217.19

9.30

  0.90

60%

23.90

2251

10.92

2433

260.99

8.62

  1.02

65%

23.89

2454

12.7

2538

303.40

8.09

  1.14

70%

23.89

2688

14.69

2650

350.94

7.66

  1.26

75%

23.82

2867

16.74

2747

398.75

7.19

  1.39

80%

23.84

3058

18.9

2830

450.58

6.79

  1.52

85%

23.78

3218

21.27

2919

505.80

6.36

  1.65

90%

23.78

3346

23.01

2960

547.18

6.12

  1.77

95%

23.78

3386

23.31

2995

554.31

6.11

  1.77

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM501 KV200

60A

P1651
16 inch straight
propeller

Multi-rotor
drone

1.6KG-2.2KG
(One axis)

4.7KG

998W

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

44.60

790

1.89

3474

84.29

9.37

0.23

40%

44.59

1002

2.58

3857

115.04

8.71

0.28

45%

44.57

1233

3.23

4201

143.96

8.56

0.33

50%

44.56

1499

4.11

4569

183.14

8.18

0.38

55%

44.56

1744

5.12

4916

228.15

7.64

0.44

60%

44.55

2015

6.2

5287

276.21

7.30

0.50

65%

44.52

2296

7.39

5606

329.00

6.98

0.56

70%

44.48

2651

8.91

5965

396.32

6.69

0.63

75%

44.49

2977

10.65

6318

473.82

6.28

0.72

80%

44.44

3295

12.47

6642

554.17

5.95

0.80

85%

44.42

3625

14.5

6966

644.09

5.63

0.88

90%

44.40

3926

16.53

7249

733.93

5.35

0.97

95%

44.38

4232

18.81

7530

834.79

5.07

1.06

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

48.19

1017

2.15

3732

103.61

9.82

0.27

40%

48.19

1246

2.79

4120

134.45

9.27

0.31

45%

48.16

1490

3.69

4502

177.71

8.38

0.38

50%

48.17

1761

4.63

4877

223.03

7.90

0.44

55%

48.14

2042

5.72

5248

275.36

7.42

0.50

60%

48.11

2339

6.88

5606

331.00

7.07

0.56

65%

48.12

2652

8.31

5957

399.88

6.63

0.64

70%

48.08

2988

10.02

6336

481.76

6.20

0.73

75%

48.08

3346

11.84

6693

569.27

5.88

0.81

80%

48.07

3689

13.93

7046

669.62

5.51

0.91

85%

47.92

4037

16.09

7362

771.03

5.24

1.00

90%

48.01

4342

18.17

7665

872.34

4.98

1.09

95%

47.93

4709

20.83

7965

998.38

4.72

1.20

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM501 KV240

40A
(4-6S)

F2280
22 inch folding
propeller

Multi-rotor,drone

1.6KG-2.2KG

(One axis)

3.89KG

794W

Load test data

Lithium Battery :6S 22,2V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

21.80

1092

3.75

1700

81.75

13.36

0.46

40%

21.79

1363

5.27

1894

114.83

11.87

0.58

45%

21.78

1599

6.83

2054

148.76

10.75

0.69

50%

21.75

1818

8.44

2202

183.57

9.90

0.80

55%

21.70

2046

10.12

2343

219.60

9.32

0.90

60%

21.72

2327

12.63

2479

274.32

8.48

1.06

65%

21.67

2582

15.1

2601

327.22

7.89

1.20

70%

21.64

2820

17.68

2724

382.60

7.37

1.34

75%

21.64

3038

20.39

2832

441.24

6.89

1.49

80%

21.58

3253

23.33

2925

503.46

6.46

1.64

85%

21.55

3418

26.22

3016

565.04

6.05

1.79

90%

21.52

3569

29.11

3095

626.45

5.70

1.93

95%

21.48

3721

31.94

3142

686.07

5.42

2.09

100%

Load test data

Lithium Battery :6S       24V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

23.60

1220

4.18

1799

98.65

12.37

0.52

40%

23.59

1497

5.78

1990

136.35

10.98

0.65

45%

23.58

1745

7.4

2149

174.49

10.0

0.78

50%

23.52

1998

9.16

2289

215.44

9.27

0.90

55%

23.50

2265

11.35

2440

266.73

8.49

1.04

60%

23.50

2510

13.59

2579

319.37

7.86

1.18

65%

23.47

2753

16.14

2715

378.81

7.27

1.33

70%

23.45

3018

19.05

2823

446.72

6.76

1.51

75%

23.39

3223

21.98

2931

514.11

6.27

1.68

80%

23.38

3425

25.05

3022

585.67

5.85

1.85

85%

23.33

3603

28.15

3097

656.74

5.49

2.03

90%

23.28

3760

31.05

3163

722.84

5.20

2.18

95%

23.25

3890

34.18

3223

794.69

4.90

2.35

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM501 KV240

40A
(4-6S)

P2275

22 inch straight propeller

Multi-rotor,drone

1.4KG-2.0KG
(One axis)

4.01KG

616M

Load test data

Lithium Battery :6S    22,2V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

21.83

866

2.56

1867

55.88

15.50

0.29

40%

21.81

1065

3.49

2082

76.12

13.99

0.35

45%

21.80

1252

4.46

2256

97.23

12.88

0.41

50%

21.81

1468

5.62

2428

122.57

11.98

0.48

55%

21.78

1706

6.98

2617

152.02

11.22

0.55

60%

21.74

1941

8.54

2801

185.66

10.45

0.63

65%

21.72

2194

10.33

2978

224.37

9.78

0.72

70%

21.71

2437

12.29

3145

266.82

9.13

0.81

75%

21.68

2682

14.24

3297

308.72

8.69

0.89

80%

21.66

2926

16.44

3438

356.09

8.22

0.99

85%

21.60

3165

18.74

3582

404.78

7.82

1.08

90%

21.59

3411

21.46

3716

463.32

7.36

1.19

95%

21.58

3611

24.01

3836

518.14

6.97

1.29

100%

Load test data

Lithium Battery :6S       24V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

23.63

1004

2.93

2018

69.24

14.50

0.33

40%

23.62

1214

3.92

2215

92.59

13.11

0.40

45%

23.60

1427

4.92

2404

116.11

12.29

0.46

50%

23.57

1671

6.24

2593

147.08

11.36

0.54

55%

23.53

1928

7.67

2793

180.48

10.68

0.62

60%

23.56

2193

9.58

2987

225.70

9.72

0.72

65%

23.52

2458

11.44

3170

269.07

9.14

0.81

70%

23.48

2744

13.63

3339

320.03

8.57

0.92

75%

23.46

3057

16.01

3480

375.59

8.14

1.03

80%

23.44

3322

18.51

3624

433.87

7.66

1.14

85%

23.40

3559

20.91

3772

489.29

7.27

1.24

90%

23.37

3792

23.73

3909

554.57

6.84

1.35

95%

23.34

4010

26.43

4027

616.88

6.50

1.46

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM501 KV240

40A
(4-6S)

P2170

21 inch straight propeller

Multi-rotor,drone

1.4KG-2.0KG
(One axis)

3.59KG

736W

Load test data

Lithium Battery :6S    22,2V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

21.82

914

3.3

1738

72.01

12.69

0.40

40%

21.81

1145

4.6

1944

100.33

11.41

0.49

45%

21.77

1351

5.89

2108

128.23

10.54

0.58

50%

21.77

1550

7.33

2257

159.57

9.71

0.68

55%

21.73

1765

8.94

2415

194.27

9.09

0.77

60%

21.69

1989

10.98

2567

238.16

8.35

0.89

65%

21.70

2216

13.15

2714

285.36

7.77

1.00

70%

21.67

2439

15.54

2851

336.75

7.24

1.13

75%

21.61

2663

18.02

2976

389.41

6.84

1.25

80%

21.60

2870

20.71

3079

447.34

6.42

1.39

85%

21.58

3062

23.48

3187

506.70

6.04

1.52

90%

21.54

3257

26.52

3267

571.24

5.70

1.67

95%

21.49

3418

29.35

3346

630.73

5.42

1.80

100%

Load test data

Lithium Battery :6S      24V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

23.60

1032

3.79

1869

89.44

11.54

  0.46

40%

23.59

1270

5.13

2061

121.02

10.49

  0.56

45%

23.55

1488

6.56

2225

154.49

9.63

  0.66

50%

23.56

1706

8.15

2384

192.01

8.88

  0.77

55%

23.54

1967

10.15

2544

238.93

8.23

  0.90

60%

23.51

2211

12.38

2698

291.05

7.60

  1.03

65%

23.48

2449

14.63

2847

343.51

7.13

  1.15

70%

23.45

2683

17.29

2980

405.45

6.62

  1.30

75%

23.42

2900

20

3108

468.40

6.19

  1.44

80%

23.37

3114

22.84

3211

533.77

5.83

  1.59

85%

23.34

3291

25.68

3313

599.37

5.49

  1.73

90%

23.32

348

28.91

3397

674.18

5.16

  1.90

95%

23.29

3594

31.61

3483

736.20

4.88

  2.02

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM501 KV310

60A
(4-6S)

F2170
21 inch folding propeller

Multi-rotor,drone

2.0KG-2.6KG
(One axis）

4.53KG

1031W

Load test data

Lithium Battery :6S

22,2V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

21.77

1517

6.77

2485

147.38

10.29

0.57

40%

21.76

1795

8.77

2693

190.84

9.41

0.68

45%

21.71

2032

10.99

2907

238.59

8.52

0.78

50%

21.70

2302

13.63

3095

295.77

7.78

0.91

55%

21.66

2573

16.57

3282

358.91

7.17

1.04

60%

21.60

2858

19.71

3460

425.74

6.71

1.18

65%

21.58

3078

22.77

3612

491.38

6.26

1.30

70%

21.54

3509

26.59

3758

572.75

6.13

1.46

75%

21.50

3649

30.3

3888

651.45

5.60

1.60

80%

21.42

3867

34.09

4005

730.21

5.30

1.74

85%

21.39

4075

38.32

4105

819.66

4.97

1.91

90%

21.38

4192

40.86

4156

873.59

4.80

2.01

95%

21.35

4202

41.59

4189

887.95

4.73

2.02

100%

Load test data

Lithium Battery :6S       24V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

23.56

1758

7.46

2660

175.76

10.00

0.63

40%

23.55

2125

9.87

2896

232.44

9.14

0.77

45%

23.52

2471

12.56

3124

295.41

8.36

0.90

50%

23.48

2783

15.36

3326

360.65

7.72

1.04

55%

23.45

3112

18.75

3526

439.69

7.08

1.19

60%

23.40

3430

22.4

3700

524.16

6.54

1.35

65%

23.34

3715

25.83

3846

602.87

6.16

1.50

70%

23.31

3908

29.83

3986

695.34

5.62

1.67

75%

23.26

4087

33.98

4116

790.37

5.17

1.83

80%

23.19

4375

37.88

4214

878.44

4.98

1.99

85%

23.15

4519

42.09

4311

974.38

4.64

2.16

90%

23.11

4540

44.23

4342

1022.16

4.44

2.25

95%

23.03

4650

45.82

4364

1055.23

4.41

2.31

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM501 KV310

40A
(4-6S)

F2075
20 inch folding propeller

Multi-rotor,drone

1.6KG-2.2KG
(One axis)

4.41KG

816W

Load test data

Lithium Battery:6S     22,2V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

21.80

1034

4.42

3149

96.36

10.73

0.29

40%

21.77

1277

5.92

3511

128.88

9.91

0.35

45%

21.76

1531

7.54

3839

164.07

9.33

0.41

50%

21.73

1783

9.37

4136

203.61

8.76

0.47

55%

21.70

2044

11.42

4423

247.81

8.25

0.54

60%

21.69

2327

13.81

4695

299.54

7.77

0.61

65%

21.67

2544

16.01

4939

346.94

7.33

0.67

70%

21.65

2812

18.72

5191

405.29

6.94

0.75

75%

21.57

3114

21.72

5421

468.50

6.65

0.83

80%

21.56

3389

24.77

5643

534.04

6.35

0.90

85%

21.52

3696

28.18

5867

606.43

6.09

0.99

90%

21.51

3965

31.25

6058

672.19

5.90

1.06

95%

21.49

3970

31.61

6067

679.30

5.84

1.07

100%

Load test data

Lithium Battery :6S       24V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

23.62

1203

5.04

3402

119.04

10.11

0.33

40%

23.58

1490

6.83

3782

161.05

9.25

0.41

45%

23.57

1762

8.68

4108

204.59

8.61

0.48

50%

23.54

2048

10.69

4414

251.64

8.14

0.54

55%

23.50

2325

12.97

4710

304.80

7.63

0.62

60%

23.48

2599

15.48

4997

363.47

7.15

0.69

65%

23.42

2878

17.93

5248

419.92

6.85

0.76

70%

23.42

3185

21.01

5498

492.05

6.47

0.85

75%

23.38

3525

24.36

5741

569.54

6.19

0.95

80%

23.32

3800

27.6

5982

643.63

5.90

1.03

85%

23.27

4117

31.6

6208

735.33

5.60

1.13

90%

23.26

4373

34.52

6393

802.94

5.45

1.20

95%

23.22

4418

35.15

6403

816.18

5.41

1.22

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM501 KV310

40A
(4-6S)

P2070
20 inch straight
propeller

Multi-rotor,drone

1.8KG-2.3KG
(One axis)

4.56KG

858W

Load test data

Lithium Battery :6S     22,2V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

21.80

1180

4.68

2680

102.02

11.57

0.36

40%

21.76

1432

6.1

2947

132.74

10.79

0.43

45%

21.74

1706

7.94

3216

172.62

9.88

0.51

50%

21.71

1969

9.92

3449

215.36

9.14

0.60

55%

21.68

2246

12.16

3697

263.63

8.52

0.68

60%

21.65

2521

14.71

3920

318.47

7.92

0.78

65%

21.65

2806

17.55

4120

379.96

7.39

0.88

70%

21.60

3074

20.15

4307

435.24

7.06

0.97

75%

21.55

3367

23.3

4493

502.12

6.71

1.07

80%

21.51

3603

26.52

4674

570.45

6.32

1.17

85%

21.50

3870

29.86

4827

641.99

6.03

1.27

90%

21.47

4085

32.71

4945

702.28

5.82

1.36

95%

21.45

4102

33.11

4962

710.21

5.78

1.37

100%

Load test data

Lithium Battery :6S       24V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

23.59

1360

5.26

2855

124.08

10.96

0.42

40%

23.57

1640

7.06

3156

166.40

9.86

0.50

45%

23.56

1965

9.16

3441

215.81

9.11

0.60

50%

23.52

2252

11.35

3700

266.95

8.44

0.69

55%

23.51

2551

13.92

3942

327.26

7.80

0.79

60%

23.45

2869

16.59

4177

389.04

7.37

0.89

65%

23.44

3135

19.52

4387

457.55

6.85

1.00

70%

23.40

3445

22.59

4579

528.61

6.52

1.10

75%

23.35

3744

25.87

4773

604.06

6.20

1.21

80%

23.31

4075

29.74

4945

693.24

5.88

1.34

85%

23.26

4295

33.33

5098

775.26

5.54

1.45

90%

23.24

4476

36.06

5210

838.03

5.34

1.54

95%

23.21

4569

36.99

5229

858.54

5.32

1.57

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM501 KV310

60A
(4-6S)

F2170
21 inch folding
propeller

multi-rotor,drone

2.0KG-2.6KG
(One axis

4.74KG

1074W

Load test data

Lithium Battery :6S    22,2V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

21.77

1517

6.77

2485

147.38

10.29

0.57

40%

21.76

1795

8.77

2693

190.84

9.41

0.68

45%

21.71

2032

10.99

2907

238.59

8.52

0.78

50%

21.70

2302

13.63

3095

295.77

7.78

0.91

55%

21.66

2573

16.57

3282

358.91

7.17

1.04

60%

21.60

2858

19.71

3460

425.74

6.71

1.18

65%

21.58

3078

22.77

3612

491.38

6.26

1.30

70%

21.54

3509

26.59

3758

572.75

6.13

1.46

75%

21.50

3649

30.3

3888

651.45

5.60

1.60

80%

21.42

3867

34.09

4005

730.21

5.30

1.74

85%

21.39

4075

38.32

4105

819.66

4.97

1.91

90%

21.38

4192

41.01

4156

876.79

4.78

2.01

95%

21.35

4202

41.59

4189

887.95

4.73

2.02

100%

Load test data

Lithium Battery :6S       24V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

23.56

1758

7.46

2660

175.76

10.00

0.63

40%

23.55

2125

9.87

2896

232.44

9.14

0.77

45%

23.52

2471

12.56

3124

295.41

8.36

0.90

50%

23.48

2783

15.36

3326

360.65

7.72

1.04

55%

23.45

3112

18.75

3526

439.69

7.08

1.19

60%

23.40

3430

22.4

3700

524.16

6.54

1.35

65%

23.34

3715

25.83

3846

602.87

6.16

1.50

70%

23.31

3908

29.83

3986

695.34

5.62

1.67

75%

23.26

4087

33.98

4116

790.37

5.17

1.83

80%

23.19

4375

37.88

4214

878.44

4.98

1.99

85%

23.15

4519

42.09

4311

974.38

4.64

2.16

90%

23.11

4530

44.01

4342

1017.07

4.45

2.24

95%

23.10

4740

46.52

4369

1074.6

4.41

2.35

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM501 KV310

40A
(4-6S)

F2075
20 inch folding
propeller

Multi-rotor,drone

1.6KG-2.2KG
(One axis)

4.41KG

816W

Load test data

Lithium Battery :6S     22,2V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

21.80

1034

4.42

3149

96.36

10.73

0.29

40%

21.77

1277

5.92

3511

128.88

9.91

0.35

45%

21.76

1531

7.54

3839

164.07

9.33

0.41

50%

21.73

1783

9.37

4136

203.61

8.76

0.47

55%

21.70

2044

11.42

4423

247.81

8.25

0.54

60%

21.69

2327

13.81

4695

299.54

7.77

0.61

65%

21.67

2544

16.01

4939

346.94

7.33

0.67

70%

21.65

2812

18.72

5191

405.29

6.94

0.75

75%

21.57

3114

21.72

5421

468.50

6.65

0.83

80%

21.56

3389

24.77

5643

534.04

6.35

0.90

85%

21.52

3696

28.18

5867

606.43

6.09

0.99

90%

21.49

3955

31.54

6043

677.79

5.84

1.07

95%

21.50

3975

31.6

6085

679.40

5.85

1.07

100%

Load test data

Lithium Battery :6S       24V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

23.62

1203

5.04

3402

119.04

10.11

0.33

40%

23.58

1490

6.83

3782

161.05

9.25

0.41

45%

23.57

1762

8.68

4108

204.59

8.61

0.48

50%

23.54

2048

10.69

4414

251.64

8.14

0.54

55%

23.50

2325

12.97

4710

304.80

7.63

0.62

60%

23.48

2599

15.48

4997

363.47

7.15

0.69

65%

23.42

2878

17.93

5248

419.92

6.85

0.76

70%

23.42

3185

21.01

5498

492.05

6.47

0.85

75%

23.38

3525

24.36

5741

569.54

6.19

0.95

80%

23.32

3800

27.6

5982

643.63

5.90

1.03

85%

23.27

4117

31.6

6208

735.33

5.60

1.13

90%

23.26

4373

34.63

6393

805.49

5.43

1.20

95%

23.22

4418

35.15

6403

816.18

5.41

1.22

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM501 KV310

40A
(4-6S)

P2070
20 inch straight
propeller

Multi-rotor,drone

1.8KG-2.3KG
(One axis)

4.56KG

861W

Load test data

Lithium Battery:6S     22,2V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

21.80

1180

4.68

2680

102.02

11.57

  0.36

40%

21.76

1432

6.1

2947

132.74

10.79

  0.43

45%

21.74

1706

7.94

3216

172.62

9.88

  0.51

50%

21.71

1969

9.92

3449

215.36

9.14

  0.60

55%

21.68

2246

12.16

3697

263.63

8.52

  0.68

60%

21.65

2521

14.71

3920

318.47

7.92

  0.78

65%

21.65

2806

17.55

4120

379.96

7.39

  0.88

70%

21.60

3074

20.15

4307

435.24

7.06

  0.97

75%

21.55

3367

23.3

4493

502.12

6.71

  1.07

80%

21.51

3603

26.52

4674

570.45

6.32

  1.17

85%

21.50

3870

29.86

4827

641.99

6.03

  1.27

90%

21.47

4080

33.04

4935

709.37

5.75

  1.37

95%

21.45

4105

33.01

4965

708.06

5.80

  1.36

100%

Load test data

Lithium Battery :6S       24V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

23.59

1360

5.26

2855

124.08

10.96

  0.42

40%

23.57

1640

7.06

3156

166.40

9.86

  0.50

45%

23.56

1965

9.16

3441

215.81

9.11

  0.60

50%

23.52

2252

11.35

3700

266.95

8.44

  0.69

55%

23.51

2551

13.92

3942

327.26

7.80

  0.79

60%

23.45

2869

16.59

4177

389.04

7.37

  0.89

65%

23.44

3135

19.52

4387

457.55

6.85

  1.00

70%

23.40

3445

22.59

4579

528.61

6.52

  1.10

75%

23.35

3744

25.87

4773

604.06

6.20

  1.21

80%

23.31

4075

29.74

4945

693.24

5.88

  1.34

85%

23.26

4295

33.33

5098

775.26

5.54

  1.45

90%

23.24

4476

36.05

5210

837.80

5.34

  1.54

95%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM501 KV360

60A
(4-6S)

F2075
20 inch folding
propeller

Multi-rotor,drone

2.2KG-2.8KG
(One axis)

4.98KG

1207W

Load test data

Lithium Battery:6S22,2V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

21.77

1588

7.4

2834

161.10

9.86

0.54

40%

21.74

1914

9.84

3106

213.92

8.95

0.66

45%

21.71

2208

12.47

3357

270.72

8.16

0.77

50%

21.67

2515

15.53

3591

336.54

7.47

0.89

55%

21.64

2838

18.99

3798

410.94

6.91

1.03

60%

21.60

3135

22.54

4008

486.86

6.44

1.16

65%

21.56

3417

26.15

4185

563.79

6.06

1.29

70%

21.50

3727

30.16

4364

648.44

5.75

1.42

75%

21.46

3876

34.88

4507

748.52

5.18

1.59

80%

21.40

4112

38.87

4649

831.82

4.94

1.7

85%

21.33

4255

43.51

4784

928.07

4.58

1.85

90%

21.32

4535

47.06

4866

1003.32

4.52

1.97

95%

21.29

4676

48.84

4888

1039.80

4.50

2.03

100%

Load test data

Lithium Battery :6S      24V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

23.54

1807

8.33

3042

196.09

9.22

0.62

40%

23.53

2196

11.12

3331

261.65

8.39

0.75

45%

23.50

2499

14.1

3582

331.35

7.54

0.88

50%

23.46

2886

17.55

3829

411.72

7.01

1.03

55%

23.42

3185

21.26

4054

497.91

6.40

1.17

60%

23.37

3578

25.29

4256

591.03

6.05

1.33

65%

23.32

3865

29.37

4432

684.91

5.64

1.48

70%

23.28

4136

33.87

4609

788.49

5.25

1.63

75%

23.21

4318

38.36

4763

890.34

4.85

1.79

80%

23.16

4504

43.04

4894

996.81

4.52

1.95

85%

23.11

4624

48.37

5008

1117.83

4.14

2.13

90%

23.05

4853

52.01

5032

1198.83

4.05

2.28

95%

23.04

4986

53.73

5080

1237.94

4.03

2.33

100%

Power configuration Measured data

Motor

ESC

Propeller

Applicable
models

Applicable

Takeoff weight

Max thrust

Max power

FM501 KV360

60A
(4-6S)

P207

20 inch straight
propeller

Multi-rotor,drone

2.0KG-2.8KG
(One axis)

5.1KG

1120

Load test data

Lithium Battery :6S    22,2V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

21.79

1397

6.28

2943

136.84

10.21

0.44

40%

21.75

1716

8.4

3250

182.70

9.39

0.54

45%

21.71

2040

10.94

3532

237.51

8.59

0.64

50%

21.69

2372

13.61

3782

295.20

8.04

0.75

55%

21.66

2706

16.61

4031

359.77

7.52

0.85

60%

21.63

3030

19.91

4251

430.65

7.04

0.97

65%

21.60

3325

23.29

4446

503.06

6.61

1.08

70%

21.54

3650

26.99

4649

581.36

6.28

1.19

75%

21.51

3923

30.92

4833

665.09

5.90

1.31

80%

21.45

4204

34.9

4991

748.61

5.62

1.43

85%

21.38

4429

39.66

5153

847.93

5.22

1.57

90%

21.34

4570

43.03

5235

918.26

4.98

1.68

95%

21.31

4615

43.85

5292

934.44

4.94

1.69

100%

Load test data

Lithium Battery :6S       24V

Voltage(V)

Thrust(g）

Current(A)

RPM

Power(W)

Efficien
cy(g/W

Torque
(N.m)

Accelerator

23.58

1588

7.14

3154

168.36

   9.43

  0.51

40%