P50M
P50M
Integrated Propulsion System
Automotive-Grade
System Design
Software
Adopts a rigorous modular design.
Fully lsolated Design Architecture
The hardware system implements a fully isolated design
architecture with high-voltage power circuits,
low-voltage signal circuits, and protective earthing(PE)
ensuring reliable data transmission,
stable equipment operation, and enhanced safety for
both personneland systems.
Dual Redundancy Design
of Position Sensor
  • Obtains PRM information in real time through dual channels
  • to meet airworthiness certification requirements
  • and flexibly respond to future regulatory requirements.
High-Specification Materials
with High Reliability
ESC
The electric speed controller (ESC)
uses automotive-grade components
with higher temperature resistance.
Motor
The motor is made of high temperature
resistant material, combined with the
dual design of knurl shaft and screws
to avoid loosening.
Propeller
The propeller adopts carbon
fiber molding process.
Automotive-Grade
Connectors
Both high-voltage and low-voltage
signal connectors are constructed with
automotive-grade materials, featuring
fool-proof design, prevention of poor
contact, and vibration resistance.
This ensures reliable system
connectivity and extended service life.
Swipe left to view all
Dual Bus Communication Protocols and
Triple Throttle Control Modes
Supports dual bus communication protocols: CAN and RS485.
Triple throttle control modes are as follows:

1

PWM+CAN digital throttle
is the default configuration

2

PWM+RS485
is optional

3

CAN+RS485
is optional
It is compatible with most flight controller (FC) communication protocols, enabling real-time data transmission and continuous monitoring of critical flight parameters (including RPM, throttle position, current, voltage and temperature). This integrated solution enables rapid data analysis, prompt response to issues, and significantly enhancing flight safety.
Sensor-Driven Redundant Back up System for
Enhanced Safety Assurance

A physical RPM sensor is used to directly obtain the RPM signal for motor control

The dual signal channels enable real-time switching to
enhance the reliability of the propulsion system

Without a physical RPM sensor, the RPM signal is obtained through software algorithms.

2000V-rated insulation and withstand voltage design,
verified by over 1000 hours of continuous aging testing,
ensures maintenance-free operation throughout its entire lifecycle
The motors, ESCs, and propellers are independently
developed and designed by HOBBYWING,
ensuring meticulous attention to every detail
The black box functionality provides
millisecond-level recording of real-time operational data,
enabling comprehensive traceability analysis
  • The fault storage function records operational fault codes during operation,
  • enabling precise root cause tracing.
  • The system continuously records the drone's operational data for 2-48 hours,
  • facilitating comprehensive post-flight data analysis.
Rapid Parameter Tuning and
Firmware OTA Updates
  • With HOBBYWING’s proprietary host computer software (DataLink),
  • users can adjust drive parameters, motor direction,
  • and LED color (default green) effortlessly to optimize flight performance and upgrade the latest firmware.
Extensive Flight Controller
Compatibility
Compatible with mainstream flight controller systems such as
ArduPilot open-source ecosystem, VK, Byaero and Jiyi, supports CAN communication,
and builds an intelligent flight ecosystem.
Real-time Detection and
Feedback of Coil Temperature
Real-time monitoring of motor temperature rise, ensuring safe flight.
View temperature data through DataLink
Thank you for your interest in HOBBYWING propulsion systems! For customized solutions,
please provide your contact information and technical requirements,
and we will get in touch with you within 24 hours.
captcha
By submitting this form, you agree to HOBBYWING's Privacy Policy
Thanks for reaching out!We have received your message and will get back to you shortly.
Best Regards,
HOBBYWING Team
P50M ESC CAD
P50MMotor CAD
P50M LED Outline CAD
54*23" CAD
64*20" CAD
Product Name
P50M
Specifications
Model P50M
Max Thrust 104kg
Recommended takeoff weight per axis 50kg
Efficiency of recommended takeoff weight 7.1g/W
Input voltage 280~450V DC
Rated voltage 400V
Lithium compatible 96~107S(LiPo)
Tube outer diameter φ60mm
Weight(with cable and Props) 6.1~6.3kg
Cable specification Power cable: 10AWG*400mm, Signal cable: 800mm
Operating temperature -35~55℃
Ingress protection IP35
* Normal flight operating voltage range: 280 VDC - 450 VDC
Hovering thrust operating voltage range: 315 VDC - 450 VDC
Maximum thrust operating voltage range: 336 VDC - 450 VDC
ESC specification
Model 80A-FOC
Communication protocol UAVCAN / RS485
ESC size 225.6*98*60mm (With connector)
Weight (INCL cable) 1200g
Peak current 80A(3s)
Continuous current 40A
Ingress Protection IP67
Throttle signal combination CAN+RS485 / CAN+PWM / RS485+PWM
Operating pulse width (Calibration not supported) 1100~1940μs
Black box 2~48h data storage
Motor specification
Model 15635
KV 9KV / 11 KV
Motor diameter Φ167.1*H100.5mm
Slot& Pole 36N 42P
Ingress Protection IPX5
Weight (INCL wire) 4250±30g
Propeller
Model 64x20" / 54x23"
Weight 860g / 707g
Material of Props Carbon non-folding Props
Mounting dimensions D60-6*M6, centre hole D20
64x20"-9KV Load performance parameters
64x20"-9KV Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature℃

400V

64x20"

35%

18099

4.9

1941.3

1153

9.3

10.50

92℃

37%

20158

5.6

2231.4

1210

9.0

12.04

39%

24258

6.9

2766.3

1314

8.8

14.74

42%

27941

8.1

3233.5

1400

8.6

16.91

45%

33804

10.1

4026.0

1525

8.4

20.20

48%

39750

12.4

4963.7

1643

8.0

23.67

51%

46459

15.6

6242.0

1769

7.5

28.00

54%

51849

18.6

7450.9

1868

7.0

31.82

57%

56043

21.2

8497.8

1945

6.6

34.99

60%

62207

25.5

10183.0

2057

6.1

39.82

63%

65772

28.1

11222.9

2121

5.9

42.66

66%

69844

31.1

12455.2

2194

5.6

45.87

69%

73789

34.2

13682.1

2263

5.4

48.91

72%

77704

37.3

14920.9

2330

5.2

51.81

75%

82332

41.0

16401.0

2405

5.0

55.06

78%

85705

43.7

17485.7

2456

4.9

57.29

81%

89805

47.0

18809.1

2514

4.8

59.89

84%

93866

50.3

20130.2

2564

4.7

62.37

87%

98297

54.0

21596.4

2610

4.6

65.08

90%

99987

55.4

22166.9

2625

4.5

66.15

100%

104197

59.1

23633.3

2654

4.4

69.02

The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, the motor temperature is 65% and the throttle runs for 10 minutes, for reference only.
54x23"-11KV Load performance parameters
54x23"-11KV Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature℃

400V

54x23"

33%

20087

6.4

2554.1

1501

7.9

12.91

90℃

35%

23100

7.5

3003.4

1604

7.7

14.60

37%

26227

8.8

3538.8

1705

7.4

16.45

39%

29462

10.4

4150.7

1804

7.1

18.45

42%

34501

13.0

5190.7

1947

6.6

21.65

45%

39734

15.9

6348.7

2082

6.3

25.01

48%

45121

19.0

7598.3

2209

5.9

28.45

51%

50614

22.3

8921.6

2329

5.7

31.92

54%

56159

25.8

10310.3

2441

5.4

35.38

57%

61698

29.4

11762.9

2546

5.2

38.81

60%

67169

33.2

13280.1

2646

5.1

42.21

63%

72509

37.1

14859.2

2741

4.9

45.57

66%

77654

41.2

16488.2

2830

4.7

48.87

69%

82538

45.4

18142.8

2913

4.5

52.08

72%

87101

49.5

19786.2

2989

4.4

55.12

75%

91282

53.4

21372.3

3057

4.3

57.95

78%

95028

57.1

22850.9

3115

4.2

60.47

81%

98287

60.4

24174.2

3164

4.1

62.64

84%

101018

63.2

25301.6

3202

4.0

64.42

87%

103186

65.5

26203.5

3231

3.9

65.79

90%

104765

67.1

26861.8

3251

3.9

66.76

100%

106112

68.6

27422.8

3266

3.9

67.56

The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, the motor temperature is 65% and the throttle runs for 10 minutes, for reference only.
64x20"-9KV Load performance parameters
64x20"-9KV Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature℃

335V

64x20"

33%

20811

6.7

2254.7

1242

9.2

14.83

98℃

35%

23695

7.9

2631.3

1318

9.0

16.60

37%

26664

9.2

3090.0

1394

8.6

18.55

39%

29714

10.8

3617.8

1469

8.2

20.64

42%

34432

13.5

4512.5

1579

7.6

23.99

45%

39298

16.4

5500.5

1684

7.1

27.50

48%

44282

19.6

6557.8

1782

6.8

31.10

51%

49344

22.9

7672.6

1874

6.4

34.73

54%

54441

26.4

8844.6

1959

6.2

38.37

57%

59523

30.1

10080.0

2040

5.9

42.01

60%

64540

34.0

11385.6

2118

5.7

45.65

63%

69436

38.1

12761.4

2192

5.4

49.27

66%

74158

42.4

14195.0

2263

5.2

52.85

69%

78649

46.7

15659.4

2330

5.0

56.33

72%

82856

51.1

17113.7

2393

4.8

59.64

75%

86728

55.2

18509.0

2449

4.7

62.70

78%

90217

59.1

19795.3

2496

4.6

65.43

81%

93281

62.5

20929.1

2535

4.5

67.76

84%

95882

65.3

21879.9

2564

4.4

69.67

87%

97991

67.6

22632.2

2585

4.3

71.14

90%

99585

69.2

23184.1

2599

4.3

72.20

100%

101269

70.9

23745.4

2611

4.3

73.25

The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, the motor temperature is 65% and the throttle runs for 10 minutes, for reference only.
54x23"-11KV Load performance parameters
54x23"-11KV Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature℃

335V

54x23"

33%

20372

7.5

2506.6

1504

8.1

12.82

94℃

35%

23552

9.0

3005.9

1608

7.8

14.74

37%

26724

10.6

3561.2

1710

7.5

16.71

39%

29916

12.4

4168.0

1808

7.2

18.71

42%

34785

15.4

5169.0

1949

6.7

21.80

45%

39790

18.7

6274.1

2082

6.3

25.00

48%

44946

22.3

7479.0

2207

6.0

28.31

51%

50244

26.2

8780.2

2325

5.7

31.71

54%

55652

30.4

10174.2

2434

5.5

35.19

57%

61121

34.8

11656.7

2537

5.2

38.72

60%

66587

39.5

13220.2

2635

5.0

42.27

63%

71974

44.3

14850.7

2729

4.8

45.79

66%

77199

49.3

16525.2

2818

4.7

49.25

69%

82176

54.3

18209.0

2903

4.5

52.56

72%

86817

59.3

19857.4

2982

4.4

55.68

75%

91040

63.9

21418.3

3052

4.3

58.51

78%

94767

68.2

22838.8

3111

4.1

61.00

81%

97933

71.8

24070.8

3158

4.1

63.09

84%

100487

74.8

25076.7

3192

4.0

64.76

87%

102394

77.1

25832.4

3216

4.0

65.99

90%

103643

78.6

26328.1

3230

3.9

66.78

100%

104316

79.4

26595.4

3237

3.9

67.20

The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, the motor temperature is 65% and the throttle runs for 10 minutes, for reference only.
Support

Manuals & Documents

Disclaimer

The purpose of this website is only to introduce you to the basic situation of HOBBYWING company and product information. Unless otherwise stated, all information provided on this website should not be regarded as an offer or acceptance, and this website will not assume any binding obligations to you as a result of the provision of information. For all your requests, HOBBYWING reserves the full right to decide whether to commit or not.

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FAQ

P50M
P50M
Integrated Propulsion System
Automotive-Grade
System Design
Software
Adopts a rigorous modular design.
Fully lsolated Design Architecture
The hardware system implements a fully isolated design
architecture with high-voltage power circuits,
low-voltage signal circuits, and protective earthing(PE)
ensuring reliable data transmission,
stable equipment operation, and enhanced safety for
both personneland systems.
Dual Redundancy Design
of Position Sensor
  • Obtains PRM information in real time through dual channels
  • to meet airworthiness certification requirements
  • and flexibly respond to future regulatory requirements.
High-Specification Materials
with High Reliability
ESC
The electric speed controller (ESC)
uses automotive-grade components
with higher temperature resistance.
Motor
The motor is made of high temperature
resistant material, combined with the
dual design of knurl shaft and screws
to avoid loosening.
Propeller
The propeller adopts carbon
fiber molding process.
Automotive-Grade
Connectors
Both high-voltage and low-voltage
signal connectors are constructed with
automotive-grade materials, featuring
fool-proof design, prevention of poor
contact, and vibration resistance.
This ensures reliable system
connectivity and extended service life.
Swipe left to view all
Dual Bus Communication Protocols and
Triple Throttle Control Modes
Supports dual bus communication protocols: CAN and RS485.
Triple throttle control modes are as follows:

1

PWM+CAN digital throttle
is the default configuration

2

PWM+RS485
is optional

3

CAN+RS485
is optional
It is compatible with most flight controller (FC) communication protocols, enabling real-time data transmission and continuous monitoring of critical flight parameters (including RPM, throttle position, current, voltage and temperature). This integrated solution enables rapid data analysis, prompt response to issues, and significantly enhancing flight safety.
Sensor-Driven Redundant Back up System for
Enhanced Safety Assurance

A physical RPM sensor is used to directly obtain the RPM signal for motor control

The dual signal channels enable real-time switching to
enhance the reliability of the propulsion system

Without a physical RPM sensor, the RPM signal is obtained through software algorithms.

2000V-rated insulation and withstand voltage design,
verified by over 1000 hours of continuous aging testing,
ensures maintenance-free operation throughout its entire lifecycle
The motors, ESCs, and propellers are independently
developed and designed by HOBBYWING,
ensuring meticulous attention to every detail
The black box functionality provides
millisecond-level recording of real-time operational data,
enabling comprehensive traceability analysis
  • The fault storage function records operational fault codes during operation,
  • enabling precise root cause tracing.
  • The system continuously records the drone's operational data for 2-48 hours,
  • facilitating comprehensive post-flight data analysis.
Rapid Parameter Tuning and
Firmware OTA Updates
  • With HOBBYWING’s proprietary host computer software (DataLink),
  • users can adjust drive parameters, motor direction,
  • and LED color (default green) effortlessly to optimize flight performance and upgrade the latest firmware.
Extensive Flight Controller
Compatibility
Compatible with mainstream flight controller systems such as
ArduPilot open-source ecosystem, VK, Byaero and Jiyi, supports CAN communication,
and builds an intelligent flight ecosystem.
Real-time Detection and
Feedback of Coil Temperature
Real-time monitoring of motor temperature rise, ensuring safe flight.
View temperature data through DataLink
Thank you for your interest in HOBBYWING propulsion systems! For customized solutions, please provide your contact information and technical requirements, and we will get in touch with you within 24 hours.
captcha
By submitting this form, you agree to HOBBYWING's Privacy Policy
Thanks for reaching out!We have received your message and will get back to you shortly.
Best Regards,
HOBBYWING Team
P50M ESC CAD
P50MMotor CAD
P50M LED Outline CAD
54*23" CAD
64*20" CAD
Product Name
P50M
Specifications
Model P50M
Max Thrust 104kg
Recommended takeoff weight per axis 50kg
Efficiency of recommended takeoff weight 7.1g/W
Input voltage 280~450V DC
Rated voltage 400V
Lithium compatible 96~107S(LiPo)
Tube outer diameter φ60mm
Weight(with cable and Props) 6.1~6.3kg
Cable specification Power cable: 10AWG*400mm, Signal cable: 800mm
Operating temperature -35~55℃
Ingress protection IP35
* Normal flight operating voltage range: 280 VDC - 450 VDC
Hovering thrust operating voltage range: 315 VDC - 450 VDC
Maximum thrust operating voltage range: 336 VDC - 450 VDC
ESC specification
Model 80A-FOC
Communication protocol UAVCAN / RS485
ESC size 225.6*98*60mm (With connector)
Weight (INCL cable) 1200g
Peak current 80A(3s)
Continuous current 40A
Ingress Protection IP67
Throttle signal combination CAN+RS485 / CAN+PWM / RS485+PWM
Operating pulse width (Calibration not supported) 1100~1940μs
Black box 2~48h data storage
Motor specification
Model 15635
KV 9KV / 11 KV
Motor diameter Φ167.1*H100.5mm
Slot& Pole 36N 42P
Ingress Protection IPX5
Weight (INCL wire) 4250±30g
Propeller
Model 64x20" / 54x23"
Weight 860g / 707g
Material of Props Carbon non-folding Props
Mounting dimensions D60-6*M6, centre hole D20
64x20"-9KV Load performance parameters
64x20"-9KV Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature℃

400V

64x20"

35%

18099

4.9

1941.3

1153

9.3

10.50

92℃

37%

20158

5.6

2231.4

1210

9.0

12.04

39%

24258

6.9

2766.3

1314

8.8

14.74

42%

27941

8.1

3233.5

1400

8.6

16.91

45%

33804

10.1

4026.0

1525

8.4

20.20

48%

39750

12.4

4963.7

1643

8.0

23.67

51%

46459

15.6

6242.0

1769

7.5

28.00

54%

51849

18.6

7450.9

1868

7.0

31.82

57%

56043

21.2

8497.8

1945

6.6

34.99

60%

62207

25.5

10183.0

2057

6.1

39.82

63%

65772

28.1

11222.9

2121

5.9

42.66

66%

69844

31.1

12455.2

2194

5.6

45.87

69%

73789

34.2

13682.1

2263

5.4

48.91

72%

77704

37.3

14920.9

2330

5.2

51.81

75%

82332

41.0

16401.0

2405

5.0

55.06

78%

85705

43.7

17485.7

2456

4.9

57.29

81%

89805

47.0

18809.1

2514

4.8

59.89

84%

93866

50.3

20130.2

2564

4.7

62.37

87%

98297

54.0

21596.4

2610

4.6

65.08

90%

99987

55.4

22166.9

2625

4.5

66.15

100%

104197

59.1

23633.3

2654

4.4

69.02

The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, the motor temperature is 65% and the throttle runs for 10 minutes, for reference only.
54x23"-11KV Load performance parameters
54x23"-11KV Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature℃

400V

54x23"

33%

20087

6.4

2554.1

1501

7.9

12.91

90℃

35%

23100

7.5

3003.4

1604

7.7

14.60

37%

26227

8.8

3538.8

1705

7.4

16.45

39%

29462

10.4

4150.7

1804

7.1

18.45

42%

34501

13.0

5190.7

1947

6.6

21.65

45%

39734

15.9

6348.7

2082

6.3

25.01

48%

45121

19.0

7598.3

2209

5.9

28.45

51%

50614

22.3

8921.6

2329

5.7

31.92

54%

56159

25.8

10310.3

2441

5.4

35.38

57%

61698

29.4

11762.9

2546

5.2

38.81

60%

67169

33.2

13280.1

2646

5.1

42.21

63%

72509

37.1

14859.2

2741

4.9

45.57

66%

77654

41.2

16488.2

2830

4.7

48.87

69%

82538

45.4

18142.8

2913

4.5

52.08

72%

87101

49.5

19786.2

2989

4.4

55.12

75%

91282

53.4

21372.3

3057

4.3

57.95

78%

95028

57.1

22850.9

3115

4.2

60.47

81%

98287

60.4

24174.2

3164

4.1

62.64

84%

101018

63.2

25301.6

3202

4.0

64.42

87%

103186

65.5

26203.5

3231

3.9

65.79

90%

104765

67.1

26861.8

3251

3.9

66.76

100%

106112

68.6

27422.8

3266

3.9

67.56

The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, the motor temperature is 65% and the throttle runs for 10 minutes, for reference only.
64x20"-9KV Load performance parameters
64x20"-9KV Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature℃

335V

64x20"

33%

20811

6.7

2254.7

1242

9.2

14.83

98℃

35%

23695

7.9

2631.3

1318

9.0

16.60

37%

26664

9.2

3090.0

1394

8.6

18.55

39%

29714

10.8

3617.8

1469

8.2

20.64

42%

34432

13.5

4512.5

1579

7.6

23.99

45%

39298

16.4

5500.5

1684

7.1

27.50

48%

44282

19.6

6557.8

1782

6.8

31.10

51%

49344

22.9

7672.6

1874

6.4

34.73

54%

54441

26.4

8844.6

1959

6.2

38.37

57%

59523

30.1

10080.0

2040

5.9

42.01

60%

64540

34.0

11385.6

2118

5.7

45.65

63%

69436

38.1

12761.4

2192

5.4

49.27

66%

74158

42.4

14195.0

2263

5.2

52.85

69%

78649

46.7

15659.4

2330

5.0

56.33

72%

82856

51.1

17113.7

2393

4.8

59.64

75%

86728

55.2

18509.0

2449

4.7

62.70

78%

90217

59.1

19795.3

2496

4.6

65.43

81%

93281

62.5

20929.1

2535

4.5

67.76

84%

95882

65.3

21879.9

2564

4.4

69.67

87%

97991

67.6

22632.2

2585

4.3

71.14

90%

99585

69.2

23184.1

2599

4.3

72.20

100%

101269

70.9

23745.4

2611

4.3

73.25

The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, the motor temperature is 65% and the throttle runs for 10 minutes, for reference only.
54x23"-11KV Load performance parameters
54x23"-11KV Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N-m)

Temperature℃

335V

54x23"

33%

20372

7.5

2506.6

1504

8.1

12.82

94℃

35%

23552

9.0

3005.9

1608

7.8

14.74

37%

26724

10.6

3561.2

1710

7.5

16.71

39%

29916

12.4

4168.0

1808

7.2

18.71

42%

34785

15.4

5169.0

1949

6.7

21.80

45%

39790

18.7

6274.1

2082

6.3

25.00

48%

44946

22.3

7479.0

2207

6.0

28.31

51%

50244

26.2

8780.2

2325

5.7

31.71

54%

55652

30.4

10174.2

2434

5.5

35.19

57%

61121

34.8

11656.7

2537

5.2

38.72

60%

66587

39.5

13220.2

2635

5.0

42.27

63%

71974

44.3

14850.7

2729

4.8

45.79

66%

77199

49.3

16525.2

2818

4.7

49.25

69%

82176

54.3

18209.0

2903

4.5

52.56

72%

86817

59.3

19857.4

2982

4.4

55.68

75%

91040

63.9

21418.3

3052

4.3

58.51

78%

94767

68.2

22838.8

3111

4.1

61.00

81%

97933

71.8

24070.8

3158

4.1

63.09

84%

100487

74.8

25076.7

3192

4.0

64.76

87%

102394

77.1

25832.4

3216

4.0

65.99

90%

103643

78.6

26328.1

3230

3.9

66.78

100%

104316

79.4

26595.4

3237

3.9

67.20

The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, the motor temperature is 65% and the throttle runs for 10 minutes, for reference only.
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