Recommended multi-rotor takeoff weight

1.5KG-2.0KG/shaft

Applicable lithium battery

6S

Applicable ambient temperature

-20℃~65℃

Power combination total weight

330g

Applicable pipe diameter of motor base

φ25mm

Length of positive and negative leads

500mm

Positive and negative plug models

XT60H-M

Signal lead length

600mm

Weight

190g

Stator core size

φ50*10mm

Dimensions

φ55.6*29mm

Spindle diameter

IN:φ6mm  OUT:φ4 mm

Dynamic balance standard

≤8mg

ESC

FOC6S60A

Driving mode

FOC sine wave

Support lithium battery

6S

PWM throttle pulse width

1100us-1900us

PWMinput frequency

50Hz-500Hz

PWMinput level

3.3V/5V

Working temperature

-20℃~65℃

Structure

Folding paddle

Length

L457 mm 18 inches

Weight

50g/piece（Propeller seat)

Single blade

19g

motor

ESC

propeller

Applicable models

Applicable takeoff weight

max pull

Max power

EA501（5010）KV310

FOC 6S60A

UP1855 18 inch folding paddle

multi-rotor drone

1.5KG-2.0KG uniaxial
(single-axis)

4.5KG

927W

Load test data

Lithium Battery： 6S

Voltage (V)

Pulling Force（g）

Current (A)

RPM

Power (W)

Efficiency (g/W)

Torque (N.m)

accelerator

22.94

1141

4.23

2987

97.04

11.76

0.25

0.4

22.95

1420

5.93

3323

136.09

10.43

0.32

0.45

22.93

1687

7.65

3640

175.41

9.62

0.38

0.5

22.89

1962

9.8

3946

224.32

8.75

0.44

0.55

22.83

2278

12.18

4235

278.07

8.19

0.51

0.6

22.8

2563

14.8

4507

337.44

7.6

0.58

0.65

22.73

2889

17.84

4763

405.5

7.12

0.65

0.7

22.67

3215

21.09

5008

478.11

6.72

0.73

0.75

22.66

3538

25.08

5248

568.31

6.23

0.81

0.8

22.58

3850

29.19

5469

659.11

5.84

0.88

0.85

22.56

4161

33.18

5680

748.54

5.56

0.94

0.9

22.46

4364

37.53

5819

842.92

5.18

0.99

0.95

22.4

4504

41.39

5851

927.14

4.86

1.03

1

Recommended multi-rotor takeoff weight

4.5KG-6.0KG/shaft

Applicable lithium battery

12-14S

Applicable ambient temperature

-20℃~65℃

Power combination total weight

722g

Applicable pipe diameter of motor base

φ30mm

Length of positive and negative leads

950mm

Signal lead length

1050mm

Weight

430g

Stator core size

φ62*18mm

Dimensions

φ68.8*34mm

Spindle diameter

IN:φ6mm  OUT:φ6mm

Dynamic balance standard

≤10mg

Support lithiumbattery

12S-14S

PWM throttle pulse width

1100us-1900us

PWM input frequency

50Hz-500Hz

PWM inputlevel

3.3V/5V

Communication interface

CAN

Yellow: CANH-1, Blue: CANL-2

Working temperature

-20°C~65°℃

motor

ESC

propeller

Applicable models

Applicable takeoff weight

max pull

Max power

EA608 KV310

FOC 14S60A

UP2480 24 inch folding paddle

multi-rotor drone

4.5KG-6.0KG uniaxial
(single-axis)

11.4KG

2532W

Load test data

Lithium Battery： 12S

Voltage (V)

Pulling Force（g）

Current (A)

RPM

Power (W)

Efficiency (g/W)

Torque (N.m)

accelerator

45.97

2980

6.36

2695

292.37

10.19

0.86

40%

45.9

3670

8.71

2995

399.79

9.18

1.05

45%

45.83

4393

11.41

3275

522.92

8.4

1.27

50%

45.78

5134

14.62

3538

669.3

7.67

1.51

55%

45.69

5924

18.2

3788

831.56

7.12

1.75

60%

45.64

6675

22.28

4027

1016.86

6.56

2

65%

45.55

7347

26.45

4247

1204.8

6.1

2.24

70%

45.54

8150

31.56

4464

1437.24

5.67

2.5

75%

45.42

8905

36.96

4664

1678.72

5.3

2.76

80%

45.36

9758

43.37

4855

1967.26

4.96

3.06

85%

45.28

10511

49.56

5038

2244.08

4.68

3.35

90%

45.22

11066

54.02

5178

2442.78

4.53

3.54

95%

45.19

11425

56.04

5197

2532.45

4.51

3.43

100%

Recommended multi-rotor takeoff weight

11KG-14KG/shaft

Applicable lithium battery

12-14S

Applicable ambient temperature

-20℃~65℃

Power combination total weight

1740g

Applicable pipe diameter of motor base

φ40mm  φ45mm

Weight

855g

Stator core size

φ138*30mm

Dimensions

φ147.6*60.4mm

Spindle diameter

IN:φ15 mm  OUT:φ10mm

Dynamic balance standard

≤15mg

Support lithiumbattery

12S-14S

PWM throttle pulse width

1100us-1900us

PWM input frequency

50Hz-500Hz

PWM inputlevel

3.3V/5V

Communication interface

CAN*2(CAN2.0B,1M bps)

Size(L*S*H)

117*67*37mm

Weight

395g

Working temperature

-20°C~65°℃

Class of protection

IPX7

motor

ESC

propeller

Applicable models

Applicable takeoff weight

max pull

Max power

EA115 KV110

FOC 14150A

UP34128 34 inch folding paddle

multi-rotor drone

11KG-14KG uniaxial
(single-axis)

25.3KG

6053W

Load test data

Lithium Battery： 14S

Voltage (V)

Pulling Force（g）

Current (A)

RPM

Power (W)

Efficiency (g/W)

Torque (N.m)

accelerator

53.56

6128

11.15

1946

597.19

10.26

2.93

40%

53.53

7466

15.24

2180

815.8

9.15

3.57

45%

53.44

9024

20.56

2408

1098.73

8.21

4.36

50%

53.38

11242

28.13

2635

1501.58

7.49

5.44

55%

53.3

12964

35.46

2843

1890.02

6.86

6.35

60%

53.18

14827

43.35

3049

2305.35

6.43

7.22

65%

53.07

16315

51.98

3251

2758.58

5.91

8.1

70%

52.96

18605

62.84

3448

3328.01

5.59

9.22

75%

52.81

20329

74.11

3632

3913.75

5.19

10.29

80%

52.68

21981

87.13

3822

4590.01

4.79

11.47

85%

52.47

23654

101.45

3999

5323.08

4.44

12.71

90%

52.31

25209

114.01

4169

5963.86

4.23

13.66

95%

52.3

25344

115.75

4156

6053.73

4.19

13.91

100%

motor

ESC

propeller

Applicable models

Applicable takeoff weight

max pull

Max power

EA115 KV110

FOC 14150A

UP36120 36 inch folding paddle

multi-rotor drone

11KG-14KG uniaxial
(single-axis)

27KG

6178W

Load test data

Lithium Battery： 14S

Voltage (V)

Pulling Force（g）

Current (A)

RPM

Power (W)

Efficiency (g/W)

Torque (N.m)

accelerator

53.49

8512

17.25

2227

922.7

9.23

3.96

40%

53.42

10189

22.77

2445

1216.37

8.38

4.75

45%

53.33

11994

28.87

2640

1539.64

7.79

5.57

50%

53.3

13372

35.26

2834

1879.36

7.12

6.33

55%

53.3

14518

40.81

2998

2175.17

6.67

6.93

60%

53.14

16017

47.18

3161

2507.15

6.39

7.57

65%

53.03

18143

56.42

3300

2991.95

6.06

8.66

70%

52.88

19352

64.49

3452

3410.23

5.67

9.43

75%

52.79

21093

74.79

3582

3948.16

5.34

10.53

80%

52.68

22280

84.49

3708

4450.93

5.01

11.46

85%

52.54

23969

93.41

3827

4907.76

4.88

12.25

90%

52.34

25903

107.53

3938

5628.12

4.6

13.65

95%

52.25

27011

118.25

4005

6178.56

4.37

14.73

100%

motor

ESC

propeller

Applicable models

Applicable takeoff weight

max pull

Max power

EA115 KV88

FOC 14150A

UP40132 40 inch folding paddle

multi-rotor drone

11KG-15KG uniaxial
(single-axis)

26.2KG

5861W

Load test data

Lithium Battery： 14S

Voltage (V)

Pulling Force（g）

Current (A)

RPM

Power (W)

Efficiency (g/W)

Torque (N.m)

accelerator

53.49

9776

19.41

2082

1038.24

9.42

4.07

40%

53.33

11652

25.75

2275

1373.25

8.48

4.97

45%

53.32

13354

31.9

2456

1700.91

7.85

5.73

50%

53.21

14956

39.57

2619

2105.52

7.1

6.57

55%

53.11

17208

48.45

2767

2573.18

6.69

7.46

60%

53.07

19250

57.82

2915

3068.51

6.27

8.42

65%

52.86

20766

67.79

3046

3583.38

5.8

9.1

70%

52.69

22715

77.28

3161

4071.88

5.58

9.97

75%

52.65

23987

88.9

3275

4680.59

5.12

10.81

80%

52.44

25435

100.68

3394

5279.66

4.82

11.48

85%

52.41

26580

110.96

3477

5815.41

4.57

12.05

90%

52.34

26605

111.97

3469

5860.51

4.54

12.11

95%

52.31

26206

112.06

3469

5861.86

4.47

12.11

100%

Recommended multi-rotor takeoff weight

15KG-18KG/shaft

Applicable lithium battery

14S

Applicable ambient temperature

-20℃~65℃

Power combination total weight

2.25KG (@ UP40132 folding paddle)
2.32KG(@ UP403135 folding paddle)

Applicable pipe diameter of motor base

φ40mm  φ45mm

Recommended multi-rotor takeoff weight

15KG-18KG/shaft

Applicable lithium battery

14S

Applicable ambient temperature

-20℃~65℃

Power combination total weight

2.55KG

Applicable pipe diameter of motor base

φ40mm  φ45mm

Weight

1280g

Stator core size

φ110*23mm

Dimensions

φ120.1*55mm

Spindle diameter

IN:φ15mm  OUT:φ10mm

Dynamic balance standard

≤15mg

Support lithiumbattery

12S-14S

PWM throttle pulse width

1100us-1900us

PWM input frequency

50Hz-500Hz

PWM inputlevel

3.3V/5V

Communication interface

CAN

Yellow: CANH-1, Blue: CANL-2

Size(L*S*H)

120*48*34mm

Working temperature

-20°C~65°℃

Class of protection

IPX7

motor

ESC

propeller

Applicable models

Applicable takeoff weight

max pull

Max power

EA126 KV85

FOC 14S230A

UP40132 40 inch folding paddle

multi-rotor drone

15KG-18KG uniaxial
(single-axis)

33KG

6.9KW

Load test data

Lithium Battery： 14S

Voltage (V)

Pulling Force（g）

Current (A)

RPM

Power (W)

Efficiency (g/W)

Torque (N.m)

accelerator

53.5

10187

21.3

2187

1139.55

8.94

4.3

40%

53.5

12415

28.3

2399

1514.05

8.2

5.2

45%

53.4

14629

35.8

2593

1911.72

7.65

6.2

50%

53.3

16720

43.9

2771

2339.87

7.15

7.1

55%

53.2

18652

52.5

2939

2793

6.68

8

60%

53.1

20902

61.9

3091

3286.89

6.36

8.9

65%

53

22945

71.9

3239

3810.7

6.02

9.9

70%

52.8

24764

81.9

3342

4324.32

5.73

10.8

75%

52.7

26769

93.1

3499

4906.37

5.46

11.7

80%

52.5

29393

107.3

3613

5633.25

5.22

12.9

85%

52.4

31201

119.2

3722

6246.08

5

13.8

90%

52.3

32573

129.8

3815

6788.54

4.8

14.5

95%

52.2

33003

132.6

3814

6921.72

4.77

14.7

100%

motor

ESC

propeller

Applicable models

Applicable takeoff weight

max pull

Max power

EA126 KV70

FOC 14S230A

UP40190 49 inch folding paddle

multi-rotor drone

15KG-18KG uniaxial
(single-axis)

38.2KG

7.7KW

Load test data

Lithium Battery： 14S

Voltage (V)

Pulling Force（g）

Current (A)

RPM

Power (W)

Efficiency (g/W)

Torque (N.m)

accelerator

53.8

8590

13.1

1260

704.78

12.19

4.5

40%

53.7

10897

18.7

1415

1004.19

10.85

5.7

45%

53.6

13480

25.8

1567

1382.88

9.75

7.2

50%

53.5

15890

33.9

1715

1813.65

8.76

8.6

55%

53.4

19343

45.1

1851

2408.34

8.03

10.5

60%

53.3

22299

55.7

1991

2968.81

7.51

12

65%

53.1

25334

68.6

2119

3642.66

6.95

13.7

70%

52.9

28311

83.4

2247

4411.86

6.42

15.4

75%

52.7

31835

102.7

2371

5412.29

5.88

17.5

80%

52.5

34639

121.7

2491

6389.25

5.42

19.1

85%

52.2

37782

144.9

2610

7563.78

5

20.9

90%

52.1

38095

147.6

2610

7689.96

4.95

20.9

95%

52.1

38285

149.3

2615

7778.53

4.92

20.9

100%

motor

ESC

propeller

Applicable models

Applicable takeoff weight

max pull

Max power

EA126 KV85

FOC 14S230A

UP43135 43 inch folding paddle

multi-rotor drone

15KG-18KG uniaxial
(single-axis)

36.1KG

8.2KW

Load test data

Lithium Battery： 14S

Voltage (V)

Pulling Force（g）

Current (A)

RPM

Power (W)

Efficiency (g/W)

Torque (N.m)

accelerator

53.4

10354

20.8

1764

1110.72

9.32

5.3

40%

53.4

13076

28.7

1953

1532.58

8.53

6.6

45%

53.3

15025

36.6

2131

1950.78

7.7

7.7

50%

53.2

17295

46.1

2297

2452.52

7.05

9

55%

53

19833

57.1

2451

3026.3

6.55

10.3

60%

52.9

22149

67.9

2600

3591.91

6.17

11.5

65%

52.7

24820

81.3

2738

4284.51

5.79

12.9

70%

52.6

26038

92.1

2869

4844.46

5.37

13.7

75%

52.4

28467

106.9

2993

5601.56

5.08

15

80%

52.3

30908

122.6

3113

6411.98

4.82

16.2

85%

52

33760

141.2

3224

7342.4

4.6

17.6

90%

51.9

35520

156.1

3279

8101.59

4.38

18.2

95%

51.8

36130

160.1

3299

8293.18

4.36

18.4

100%

Recommended multi-rotor takeoff weight

25KG-30KG/shaft

Applicable lithium battery

18S

Applicable ambient temperature

-20℃~65℃

Power combination total weight

3900g

Applicable pipe diameter of motor base

φ50mm

Weight

2180g

Stator core size

φ138*30mm

Dimensions

φ147.6*60.4mm

Spindle diameter

IN:φ15mm  OUT:φ10mm

Dynamic balance standard

≤15mg

Support lithiumbattery

48S-100S

PWM throttle pulse width

1100us-1900us

PWM input frequency

50Hz-500Hz

PWM inputlevel

3.3V/5V

Communication interface

CAN*2(CAN2.0B,1M bps)

Yellow: CANH-1, Green: CANL-1, Red: CANH-2, Blue: CANL-2

Size(L*S*H)

117*67*37mm

Weight

630g

Working temperature

-20°C~65°℃

Class of protection

IPX7

Structure

Folding paddle

Length

1425mm 56 inches

Pitch

20

Weight

862g (Including slurry seat)

motor

ESC

propeller

Applicable models

Applicable takeoff weight

max pull

Max power

EA140 KV45

FOC 18S280A

UP5620  56 inch folding paddle

multi-rotor drone

25KG-30KG uniaxial
(single-axis)

60.8KG

12.1KW

Load test data

Lithium Battery： 18S

Voltage (V)

Pulling Force（g）

Current (A)

RPM

Power (W)

Efficiency (g/W)

Torque (N.m)

accelerator

68.8

16630

21.4

1274

1472.32

11.3

11.04

40%

68.7

19917

28.3

1411

1944.21

10.24

13.16

45%

68.6

23560

36.4

1540

2497.04

9.44

15.49

50%

68.5

27528

46.1

1662

3157.85

8.72

18.15

55%

68.4

31642

57.2

1773

3912.48

8.09

21.08

60%

68.2

35091

67.8

1882

4623.96

7.59

23.47

65%

68.1

38980

79.9

1982

5441.19

7.16

26.22

70%

67.9

42722

92.7

2077

6294.33

6.79

28.94

75%

67.8

46402

108.5

2166

7356.3

6.31

32.43

80%

67.6

50121

122.5

2250

8281

6.05

35.15

85%

67.4

53234

138.7

2332

9348.38

5.69

38.28

90%

67.2

57106

156.2

2407

10496.64

5.44

41.65

95%

66.9

60892

182.2

2494

12189.18

5

46.68

100%

Recommended multi-rotor takeoff weight

40KG-45KG/shaft

Applicable lithium battery

18S

Applicable ambient temperature

-20℃~65℃

Power combination total weight

6.1KG

Applicable pipe diameter of motor base

φ60mm

Weight

3800g

Stator core size

φ180*25mm

Dimensions

φ195.4*75mm

Spindle diameter

IN:φ25mm  OUT:φ10mm

Support lithiumbattery

48S-100S

PWM throttle pulse width

1100us-1900us

PWM input frequency

50Hz-500Hz

PWM inputlevel

3.3V/5V

Communication interface

CAN*2(CAN2.0B,1M bps)

Yellow: CANH-1, Green: CANL-1, Red: CANH-2, Blue: CANL-2

Size(L*S*H)

117*67*37mm

Weight

660g

Working temperature

-20°C~65°℃

Class of protection

IPX7

Structure

Folding oar

material

Carbon fiber + nylon + aluminum alloy

Length

1613mm

Screw pitch

24

Weight

100og/ blade (with paddle clamp)
708g (Two blades）

Mounting dimension

Centre hole:φ10

Mounting hole

1：6-M5 EQS D40mm
2：4-M6 D55mm

motor

ESC

propeller

Applicable models

Applicable takeoff weight

max pull

Max power

EA185 KV36

FOC 18S280A

UP6324
63 inch folding paddle

multi-rotor drone

40KG-45KG uniaxial
(single-axis)

80.6KG

15.5KW

Load test data

Lithium Battery： 18S

Voltage (V)

Pulling Force（g）

Current (A)

RPM

Power (W)

Efficiency (g/W)

Torque (N.m)

accelerator

69.2

21646

28

1112

1937.6

11.17

14.7

40%

69

26884

39.1

1246

2697.9

9.96

18.4

45%

68.9

33240

53.2

1372

3665.48

9.07

22.8

50%

68.7

39349

69.1

1495

4747.17

8.29

27.1

55%

68.4

46304

89.5

1612

6121.8

7.56

32.3

60%

68.2

52521

110.9

1729

7563.38

6.94

36.9

65%

67.9

58220

133.1

1835

9037.49

6.44

41.2

70%

67.5

65360

163.9

1936

11063.25

5.91

47.1

75%

67.1

71503

195.7

2037

13131.47

5.45

51.1

80%

66.9

72674

202.3

2082

13533.87

5.37

52.3

85%

66.8

74195

213.2

2109

14241.76

5.21

53.5

90%

66.8

76144

219.3

2120

14649.24

5.2

54.7

95%

66.8

80620

233.1

2186

15571.08

5.18

55.5

100%