P65V
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P65V
Integrated Propulsion System
Specially Designed for Large VTOL Fixed-Wing UAVs (eVTOL)
Automotive-Grade System Design
Software
Adopts rigorous modularized design and various
redundancy strategies.
Hardware
The Protective Earth (PE) is completely isolated from the
high-voltage power circuits and low-voltage signal circuits,
ensuring superior system reliability.
Dual Redundancy Design
of the Position Sensor
The flexible setting of the propeller stopping position
Reduces the resistance of the UAV during cruise
flight and extends the flight endurance.
The propeller is aerodynamically optimized
With a large aspect ratio, a small windward side,
and a propeller tip with a low wind resistance,
striking an optimal balance between efficiency and thrust capacity.
This design is tailored for the specific application requirements of VTOLs.
Obtain RPM information in real time through dual channels
To meet airworthiness certification requirements and
easily respond to future regulatory requirements.
Dual Redundancy Design
of the Position Sensor
The flexible setting of the propeller stopping position
Reduces the resistance of the UAV during cruise
flight and extends the flight endurance.
The propeller is aerodynamically optimized
with a large aspect ratio, a small windward side,
and a propeller tip with a low wind resistance,
striking an optimal balance between efficiency and thrust capacity.
This design is tailored for the specific application requirements of VTOLs.
Obtain RPM information in real time through dual channels
to meet airworthiness certification requirements and
easily respond to future regulatory requirements.
High-Specification Materials with
High Reliability Technology Process
  • ESC
  • Motor
  • Propeller
  • Automotive-Grade Connectors
The ESC uses automotive-grade
components with higher
temperature resistance.
The motor is made of high temperature resistant material,
combined with the dual design of knurl shaft
and screws to avoid loosening.
The propeller adopts carbon fiber molding process.
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.
High-Specification Materials with
High Reliability Technology Process
ESC
The 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.
Dual Bus Communication Protocols
and Triple Throttle Control Modes
Supports dual bus communication protocols: CAN and RS485.
Provides triple throttle control modes, supports dual-protocol verification,
ensuring the safety of personnel during every debugging and testing session.
Triple throttle control modes are as follows:
CAN+RS485
is the default configuration
CAN+PWM
is optional
RS485+PWM
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 Backup
for Added Security

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

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 control systems such as
ArduPilot open-source ecosystem, VK, Byaero and Jiyi,
supports CAN communication, and builds an intelligent flight ecosystem.
Support Real-time Detection and
Feedback of Coil Temperature
Real-time monitoring of motor temperature rise, ensuring safe flight.
View Temperature Data Through Datalink
P65V-60×20"
Test Voltage: 335V

Test Voltage:400V

  • *The above data were measured at room temperature (25℃) and sea level, and the motor and ESC were under the condition of good heat dissipation.
  • The abscissa represents the maximum safe operating time at each overload point. In actual flight, if the propulsion system exceeds this time,
  • there is a high probability of irreversible failure. But for flight safety, the propulsion system will not automatically shut down.
P65V-54×23"
Test Voltage:335V

Test Voltage:400V

  • *The above data were measured at room temperature (25℃) and sea level, and the motor and ESC were under the condition of good heat dissipation.
  • The abscissa represents the maximum safe operating time at each overload point. In actual flight, if the propulsion system exceeds this time,
  • there is a high probability of irreversible failure. But for flight safety, the propulsion system will not automatically shut down.
P65V ESC CAD
P65VMotor CAD
This product implements a fully isolated design architecture with high-voltage power circuits, low-voltage signal circuits, and protective earthing (PE), ensuring a low-impedance connection (common grounding) between the motor mounting base and the housing of ESC.
P65V LED Outline CAD
54x23" CAD
60×20" CAD
Product Name
P65V Integrated Propulsion System Specifications
Specifications
Model P65V
Max Thrust 108kg
Recommended takeoff weight per axis(5min max) 65kg
Efficiency of recommended takeoff weight 5.7g/W / 5.3g/W
Input voltage 280~450V DC
Rated voltage 335V
Lithium compatible 96~107S（LiPo）
Propeller Positioning IPC (Intelligent Propeller Control)
Weight（with cable and Props） 6165±60g / 6252±60g
Cable specification Power cable: 10AWG*400mm, Signal cable: 800mm
Operating temperature -35~55℃
Ingress protection IP25
Rated power input (5min max) 13.6kW
Rated power output (5min max) 11.2kW
* Normal flight operating voltage range: 280V DC - 450V DC Hovering thrust operating voltage range: 315V DC - 450V DC Maximum thrust operating voltage range: 336V DC - 450V DC
ESC specification
Model 100A-FOC
Communication protocol UAVCAN / RS485
ESC size 225.6*98*60 mm（With Connector）
Weight（INCL cable） 1200±20g
Peak current 100A（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 11KV
Motor diameter Φ167.1*H100.5mm
Slot& Pole 36N 42P
Ingress Protection IPX5
Weight (INCL wire) 4345±20g
Motor temperature signal Standard configuration
Motor position sensor signal Standard configuration
Propeller
Model 60x20" / 54x23"
Weight 620±20g / 707±20g
Material of props Carbon non-folding props
Mounting dimensions D60-6*M6, centre hole D20
60x20"-11V Load performance parameters
60x20"-11V Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Input Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Output Power(W)

Temperature(℃)

335V

60x20"

33%

21960

8.8

2954.3

1393

7.4

13.98

2039.8

87℃

35%

24913

10.4

3470.2

1487

7.2

15.89

2473.5

37%

28098

12.0

4022.0

1580

7.0

17.89

2959.2

39%

31421

13.8

4612.3

1671

6.8

19.96

3493.3

42%

36585

16.7

5575.8

1802

6.6

23.19

4376.6

45%

41872

19.8

6636.1

1927

6.3

26.50

5346.5

48%

47196

23.3

7787.8

2043

6.1

29.86

6388.8

51%

52490

27.0

9016.5

2153

5.8

33.22

7488.5

54%

57701

30.8

10302.2

2255

5.6

36.55

8630.4

57%

62788

34.8

11623.2

2352

5.4

39.79

9799.6

60%

67722

38.8

12959.6

2443

5.2

42.94

10981.8

63%

72478

42.8

14295.7

2528

5.1

45.96

12164.5

66%

77041

46.8

15620.8

2607

4.9

48.85

13336.3

69%

81394

50.7

16928.8

2681

4.8

51.60

14488.0

72%

85524

54.6

18216.4

2749

4.7

54.22

15610.8

75%

89414

58.4

19481.5

2812

4.6

56.71

16696.8

78%

93041

62.1

20719.8

2868

4.5

59.06

17736.8

81%

96377

65.7

21921.9

2918

4.4

61.27

18719.5

84%

99383

69.2

23069.8

2961

4.3

63.32

19629.8

87%

102010

72.4

24133.2

2997

4.2

65.16

20446.9

90%

104191

75.2

25066.8

3026

4.2

66.73

21143.1

100%

107151

79.3

26420.1

3063

4.1

68.95

22117.6
The below data is based on the measurement made by Hobbywing Laboratory at room temperature 25℃, sea level altitude, varying throttle input regulation, and the temperature of the motor is recommand take off weight under continuous operation for 5 min, which is for reference only.
60x20"-11V Load performance parameters
60x20"-11V Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Input Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Output Power(W)

Temperature(℃)

400V

60x20"

33%

21641

8.0

3188.1

1394

6.8

13.67

1995.1

89℃

35%

24691

9.3

3710.1

1490

6.7

15.56

2427.3

37%

27969

10.8

4301.9

1584

6.5

17.64

2926.3

39%

31408

12.4

4951.5

1675

6.3

19.86

3483.3

42%

36748

15.0

6009.1

1805

6.1

23.32

4407.4

45%

42177

17.9

7137.9

1926

5.9

26.83

5411.3

48%

47581

20.8

8314.9

2041

5.7

30.27

6470.7

51%

52886

23.8

9526.5

2150

5.6

33.61

7568.1

54%

58042

26.9

10766.3

2254

5.4

36.83

8691.3

57%

63026

30.1

12031.8

2351

5.2

39.93

9832.2

60%

67830

33.4

13322.7

2443

5.1

42.94

10985.0

63%

72458

36.7

14638.9

2529

4.9

45.86

12145.7

66%

76922

40.0

15979.5

2609

4.8

48.72

13310.3

69%

81231

43.4

17341.4

2683

4.7

51.52

14474.0

72%

85390

46.9

18717.5

2751

4.6

54.27

15629.7

75%

89394

50.4

20094.8

2812

4.4

56.94

16766.5

78%

93219

53.8

21452.2

2868

4.3

59.50

17868.3

81%

96819

57.1

22758.5

2918

4.3

61.89

18912.4

84%

100119

60.1

23971.6

2962

4.2

64.06

19869.3

87%

103011

62.8

25038.8

2999

4.1

65.92

20702.4

90%

105346

65.0

25897.4

3029

4.1

67.38

21368.0

100%

107513

66.9

26687.5

3056

4.0

68.68

21977.9
The below data is based on the measurement made by Hobbywing Laboratory at room temperature 25℃, sea level altitude, varying throttle input regulation, and the temperature of the motor is recommand take off weight under continuous operation for 5 min, which is for reference only.
54x23"-11KV Load performance parameters
54x23"-11KV Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Input Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Output Power(W)

Temperature(℃)

400V

54x23"

33%

22319

8.4

3376.5

1535

6.6

14.48

2326.2

92℃

35%

25780

10.1

4026.9

1648

6.4

16.73

2885.4

37%

29222

11.8

4722.3

1752

6.2

18.98

3481.0

39%

32695

13.6

5461.0

1849

6.0

21.26

4116.3

42%

38040

16.6

6652.7

1988

5.7

24.75

5151.3

45%

43607

19.9

7952.2

2119

5.5

28.37

6295.0

48%

49417

23.4

9372.2

2246

5.3

32.13

7556.9

51%

55441

27.3

10929.8

2369

5.1

36.05

8944.8

54%

61615

31.6

12643.6

2490

4.9

40.13

10463.4

57%

67842

36.3

14524.4

2608

4.7

44.35

12108.5

60%

74004

41.4

16561.8

2721

4.5

48.64

13858.9

63%

79970

46.8

18711.8

2828

4.3

52.92

15667.8

66%

85600

52.2

20892.8

2924

4.1

57.02

17460.7

69%

90760

57.5

22995.0

3008

3.9

60.78

19143.9

72%

95323

62.2

24902.0

3076

3.8

64.04

20624.6

75%

99183

66.3

26516.3

3127

3.7

66.68

21833.4

78%

102257

69.4

27778.5

3163

3.7

68.66

22740.6

81%

104500

71.7

28672.4

3186

3.6

70.01

23356.7

84%

105906

73.0

29216.7

3199

3.6

70.81

23718.2

100%

106569

73.7

29468.1

3204

3.6

71.18

23881.1
The below data is based on the measurement made by Hobbywing Laboratory at room temperature 25℃, sea level altitude, varying throttle input regulation, and the temperature of the motor is recommand take off weight under continuous operation for 5 min, which is for reference only.
54x23"-11KV Load performance parameters
54x23"-11KV Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Input Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Output Power(W)

Temperature(℃)

335V

54x23"

33%

22590

9.7

3236.7

1538

7.0

14.65

2359.8

90℃

35%

26107

11.6

3877.5

1650

6.7

16.95

2929.0

37%

29542

13.5

4537.1

1753

6.5

19.19

3522.5

39%

32964

15.6

5229.4

1848

6.3

21.44

4148.3

42%

38183

19.0

6356.3

1984

6.0

24.87

5166.3

45%

43607

22.7

7620.2

2115

5.7

28.45

6301.3

48%

49290

27.0

9045.1

2243

5.4

32.23

7571.1

51%

55232

31.8

10641.3

2369

5.2

36.21

8982.6

54%

61382

37.0

12403.1

2492

4.9

40.36

10529.1

57%

67654

42.7

14308.2

2610

4.7

44.60

12188.7

60%

73932

48.7

16319.9

2722

4.5

48.85

13924.4

63%

80079

54.9

18390.1

2826

4.4

53.02

15686.7

66%

85946

61.1

20462.6

2919

4.2

56.98

17418.1

69%

91383

67.1

22475.3

3001

4.1

60.65

19059.2

72%

96245

72.7

24360.7

3071

4.0

63.92

20553.9

75%

100405

77.7

26047.5

3129

3.9

66.70

21852.1

78%

103755

82.0

27463.9

3174

3.8

68.94

22912.3

81%

106226

85.2

28545.3

3206

3.7

70.60

23703.3

84%

107786

87.3

29246.2

3227

3.7

71.64

24207.5

100%

108497

88.2

29570.4

3236

3.7

72.11

24438.5
The below data is based on the measurement made by Hobbywing Laboratory at room temperature 25℃, sea level altitude, varying throttle input regulation, and the temperature of the motor is recommand take off weight under continuous operation for 5 min, which is for reference only.
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P65V Load performance parameters
P65V ESC CAD
P65V Motor CAD
P65V LED Outline CAD
54x23" CAD
60x20" CAD
P65V Specification

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P65V
Overview Specifications Support Accessories Detail Contact us Shop
Buy
P65V
Integrated Propulsion System
Specially Designed for Large VTOL Fixed-Wing UAVs (eVTOL)
Automotive-Grade System Design
Software
Adopts rigorous modularized design and various
redundancy strategies.
Hardware
The Protective Earth (PE) is completely isolated from the
high-voltage power circuits and low-voltage signal circuits,
ensuring superior system reliability.
Dual Redundancy Design
of the Position Sensor
The flexible setting of the propeller stopping position
Reduces the resistance of the UAV during cruise
flight and extends the flight endurance.
The propeller is aerodynamically optimized
With a large aspect ratio, a small windward side,
and a propeller tip with a low wind resistance,
striking an optimal balance between efficiency and thrust capacity.
This design is tailored for the specific application requirements of VTOLs.
Obtain RPM information in real time through dual channels
To meet airworthiness certification requirements and
easily respond to future regulatory requirements.
Dual Redundancy Design
of the Position Sensor
The flexible setting of the propeller stopping position
Reduces the resistance of the UAV during cruise
flight and extends the flight endurance.
The propeller is aerodynamically optimized
with a large aspect ratio, a small windward side,
and a propeller tip with a low wind resistance,
striking an optimal balance between efficiency and thrust capacity.
This design is tailored for the specific application requirements of VTOLs.
Obtain RPM information in real time through dual channels
to meet airworthiness certification requirements and
easily respond to future regulatory requirements.
High-Specification Materials with
High Reliability Technology Process
  • ESC
  • Motor
  • Propeller
  • Automotive-Grade Connectors
The ESC uses automotive-grade
components with higher
temperature resistance.
The motor is made of high temperature resistant material,
combined with the dual design of knurl shaft
and screws to avoid loosening.
The propeller adopts carbon fiber molding process.
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.
High-Specification Materials with
High Reliability Technology Process
ESC
The 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.
Dual Bus Communication Protocols
and Triple Throttle Control Modes
Supports dual bus communication protocols: CAN and RS485.
Provides triple throttle control modes, supports dual-protocol verification,
ensuring the safety of personnel during every debugging and testing session.
Triple throttle control modes are as follows:
CAN+RS485
is the default configuration
CAN+PWM
is optional
RS485+PWM
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 Backup
for Added Security

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

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 control systems such as
ArduPilot open-source ecosystem, VK, Byaero and Jiyi,
supports CAN communication, and builds an intelligent flight ecosystem.
Support Real-time Detection and
Feedback of Coil Temperature
Real-time monitoring of motor temperature rise, ensuring safe flight.
View Temperature Data Through Datalink
P65V-60×20"
Test Voltage: 335V

Test Voltage:400V

  • *The above data were measured at room temperature (25℃) and sea level, and the motor and ESC were under the condition of good heat dissipation.
  • The abscissa represents the maximum safe operating time at each overload point. In actual flight, if the propulsion system exceeds this time,
  • there is a high probability of irreversible failure. But for flight safety, the propulsion system will not automatically shut down.
P65V-54×23"
Test Voltage:335V

Test Voltage:400V

  • *The above data were measured at room temperature (25℃) and sea level, and the motor and ESC were under the condition of good heat dissipation.
  • The abscissa represents the maximum safe operating time at each overload point. In actual flight, if the propulsion system exceeds this time,
  • there is a high probability of irreversible failure. But for flight safety, the propulsion system will not automatically shut down.
P65V ESC CAD
P65VMotor CAD
This product implements a fully isolated design architecture with high-voltage power circuits, low-voltage signal circuits, and protective earthing (PE), ensuring a low-impedance connection (common grounding) between the motor mounting base and the housing of ESC.
P65V LED Outline CAD
54x23" CAD
60×20" CAD
Product Name
P65V Integrated Propulsion System Specifications
Specifications
Model P65V
Max Thrust 108kg
Recommended takeoff weight per axis(5min max) 65kg
Efficiency of recommended takeoff weight 5.7g/W / 5.3g/W
Input voltage 280~450V DC
Rated voltage 335V
Lithium compatible 96~107S（LiPo）
Propeller Positioning IPC (Intelligent Propeller Control)
Weight（with cable and Props） 6165±60g / 6252±60g
Cable specification Power cable: 10AWG*400mm, Signal cable: 800mm
Operating temperature -35~55℃
Ingress protection IP25
Rated power input (5min max) 13.6kW
Rated power output (5min max) 11.2kW
* Normal flight operating voltage range: 280V DC - 450V DC Hovering thrust operating voltage range: 315V DC - 450V DC Maximum thrust operating voltage range: 336V DC - 450V DC
ESC specification
Model 100A-FOC
Communication protocol UAVCAN / RS485
ESC size 225.6*98*60 mm（With Connector）
Weight（INCL cable） 1200±20g
Peak current 100A（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 11KV
Motor diameter Φ167.1*H100.5mm
Slot& Pole 36N 42P
Ingress Protection IPX5
Weight (INCL wire) 4345±20g
Motor temperature signal Standard configuration
Motor position sensor signal Standard configuration
Propeller
Model 60x20" / 54x23"
Weight 620±20g / 707±20g
Material of props Carbon non-folding props
Mounting dimensions D60-6*M6, centre hole D20
60x20"-11V Load performance parameters
60x20"-11V Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Input Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Output Power(W)

Temperature(℃)

335V

60x20"

33%

21960

8.8

2954.3

1393

7.4

13.98

2039.8

87℃

35%

24913

10.4

3470.2

1487

7.2

15.89

2473.5

37%

28098

12.0

4022.0

1580

7.0

17.89

2959.2

39%

31421

13.8

4612.3

1671

6.8

19.96

3493.3

42%

36585

16.7

5575.8

1802

6.6

23.19

4376.6

45%

41872

19.8

6636.1

1927

6.3

26.50

5346.5

48%

47196

23.3

7787.8

2043

6.1

29.86

6388.8

51%

52490

27.0

9016.5

2153

5.8

33.22

7488.5

54%

57701

30.8

10302.2

2255

5.6

36.55

8630.4

57%

62788

34.8

11623.2

2352

5.4

39.79

9799.6

60%

67722

38.8

12959.6

2443

5.2

42.94

10981.8

63%

72478

42.8

14295.7

2528

5.1

45.96

12164.5

66%

77041

46.8

15620.8

2607

4.9

48.85

13336.3

69%

81394

50.7

16928.8

2681

4.8

51.60

14488.0

72%

85524

54.6

18216.4

2749

4.7

54.22

15610.8

75%

89414

58.4

19481.5

2812

4.6

56.71

16696.8

78%

93041

62.1

20719.8

2868

4.5

59.06

17736.8

81%

96377

65.7

21921.9

2918

4.4

61.27

18719.5

84%

99383

69.2

23069.8

2961

4.3

63.32

19629.8

87%

102010

72.4

24133.2

2997

4.2

65.16

20446.9

90%

104191

75.2

25066.8

3026

4.2

66.73

21143.1

100%

107151

79.3

26420.1

3063

4.1

68.95

22117.6
The below data is based on the measurement made by Hobbywing Laboratory at room temperature 25℃, sea level altitude, varying throttle input regulation, and the temperature of the motor is recommand take off weight under continuous operation for 5 min, which is for reference only.
60x20"-11V Load performance parameters
60x20"-11V Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Input Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Output Power(W)

Temperature(℃)

400V

60x20"

33%

21641

8.0

3188.1

1394

6.8

13.67

1995.1

89℃

35%

24691

9.3

3710.1

1490

6.7

15.56

2427.3

37%

27969

10.8

4301.9

1584

6.5

17.64

2926.3

39%

31408

12.4

4951.5

1675

6.3

19.86

3483.3

42%

36748

15.0

6009.1

1805

6.1

23.32

4407.4

45%

42177

17.9

7137.9

1926

5.9

26.83

5411.3

48%

47581

20.8

8314.9

2041

5.7

30.27

6470.7

51%

52886

23.8

9526.5

2150

5.6

33.61

7568.1

54%

58042

26.9

10766.3

2254

5.4

36.83

8691.3

57%

63026

30.1

12031.8

2351

5.2

39.93

9832.2

60%

67830

33.4

13322.7

2443

5.1

42.94

10985.0

63%

72458

36.7

14638.9

2529

4.9

45.86

12145.7

66%

76922

40.0

15979.5

2609

4.8

48.72

13310.3

69%

81231

43.4

17341.4

2683

4.7

51.52

14474.0

72%

85390

46.9

18717.5

2751

4.6

54.27

15629.7

75%

89394

50.4

20094.8

2812

4.4

56.94

16766.5

78%

93219

53.8

21452.2

2868

4.3

59.50

17868.3

81%

96819

57.1

22758.5

2918

4.3

61.89

18912.4

84%

100119

60.1

23971.6

2962

4.2

64.06

19869.3

87%

103011

62.8

25038.8

2999

4.1

65.92

20702.4

90%

105346

65.0

25897.4

3029

4.1

67.38

21368.0

100%

107513

66.9

26687.5

3056

4.0

68.68

21977.9
The below data is based on the measurement made by Hobbywing Laboratory at room temperature 25℃, sea level altitude, varying throttle input regulation, and the temperature of the motor is recommand take off weight under continuous operation for 5 min, which is for reference only.
54x23"-11KV Load performance parameters
54x23"-11KV Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Input Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Output Power(W)

Temperature(℃)

400V

54x23"

33%

22319

8.4

3376.5

1535

6.6

14.48

2326.2

92℃

35%

25780

10.1

4026.9

1648

6.4

16.73

2885.4

37%

29222

11.8

4722.3

1752

6.2

18.98

3481.0

39%

32695

13.6

5461.0

1849

6.0

21.26

4116.3

42%

38040

16.6

6652.7

1988

5.7

24.75

5151.3

45%

43607

19.9

7952.2

2119

5.5

28.37

6295.0

48%

49417

23.4

9372.2

2246

5.3

32.13

7556.9

51%

55441

27.3

10929.8

2369

5.1

36.05

8944.8

54%

61615

31.6

12643.6

2490

4.9

40.13

10463.4

57%

67842

36.3

14524.4

2608

4.7

44.35

12108.5

60%

74004

41.4

16561.8

2721

4.5

48.64

13858.9

63%

79970

46.8

18711.8

2828

4.3

52.92

15667.8

66%

85600

52.2

20892.8

2924

4.1

57.02

17460.7

69%

90760

57.5

22995.0

3008

3.9

60.78

19143.9

72%

95323

62.2

24902.0

3076

3.8

64.04

20624.6

75%

99183

66.3

26516.3

3127

3.7

66.68

21833.4

78%

102257

69.4

27778.5

3163

3.7

68.66

22740.6

81%

104500

71.7

28672.4

3186

3.6

70.01

23356.7

84%

105906

73.0

29216.7

3199

3.6

70.81

23718.2

100%

106569

73.7

29468.1

3204

3.6

71.18

23881.1
The below data is based on the measurement made by Hobbywing Laboratory at room temperature 25℃, sea level altitude, varying throttle input regulation, and the temperature of the motor is recommand take off weight under continuous operation for 5 min, which is for reference only.
54x23"-11KV Load performance parameters
54x23"-11KV Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Input Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Output Power(W)

Temperature(℃)

335V

54x23"

33%

22590

9.7

3236.7

1538

7.0

14.65

2359.8

90℃

35%

26107

11.6

3877.5

1650

6.7

16.95

2929.0

37%

29542

13.5

4537.1

1753

6.5

19.19

3522.5

39%

32964

15.6

5229.4

1848

6.3

21.44

4148.3

42%

38183

19.0

6356.3

1984

6.0

24.87

5166.3

45%

43607

22.7

7620.2

2115

5.7

28.45

6301.3

48%

49290

27.0

9045.1

2243

5.4

32.23

7571.1

51%

55232

31.8

10641.3

2369

5.2

36.21

8982.6

54%

61382

37.0

12403.1

2492

4.9

40.36

10529.1

57%

67654

42.7

14308.2

2610

4.7

44.60

12188.7

60%

73932

48.7

16319.9

2722

4.5

48.85

13924.4

63%

80079

54.9

18390.1

2826

4.4

53.02

15686.7

66%

85946

61.1

20462.6

2919

4.2

56.98

17418.1

69%

91383

67.1

22475.3

3001

4.1

60.65

19059.2

72%

96245

72.7

24360.7

3071

4.0

63.92

20553.9

75%

100405

77.7

26047.5

3129

3.9

66.70

21852.1

78%

103755

82.0

27463.9

3174

3.8

68.94

22912.3

81%

106226

85.2

28545.3

3206

3.7

70.60

23703.3

84%

107786

87.3

29246.2

3227

3.7

71.64

24207.5

100%

108497

88.2

29570.4

3236

3.7

72.11

24438.5
The below data is based on the measurement made by Hobbywing Laboratory at room temperature 25℃, sea level altitude, varying throttle input regulation, and the temperature of the motor is recommand take off weight under continuous operation for 5 min, which is for reference only.
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P65V Load performance parameters
P65V ESC CAD
P65V Motor CAD
P65V LED Outline CAD
54x23" CAD
60x20" CAD
P65V Specification

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