P65M - Integrated Propulsion System for Industrial Drones
P65m Integrated Propulsion System
P65M
Propulsion System
Elevated to Passenger
Car Standards
Modular Design
Software
Adopts a rigorous modular design.
High Voltage Drone Propulsion System
Fully Isolated Architecture with Protective Earthing
High-voltage power circuits, low-voltage signal circuits,
and protective earthing (PE) are completelyisolated,
delivering reliable data transmission,
stable system performance,
and superior safety for operators and equipment alike.
Dual Redundancy for
Position Sensor

Real-time RPM acquisition via dual channels,

engineered to meet current airworthiness certification standards

while preparing for future regulatory evolution.

Hobbywing P65m Powerful Drone Motor
High-Specification Materials
With High Reliability
P65m Drone Electric Speed Controller (Esc)
High-Temperature ESC with Automotive Components
The Electric Speed Controller (ESC) uses premium automotive-grade
components designed for elevated temperature resistance.
P65m Powerful Drone Motor
High-Reliability Motor Design
Built with high-temperature resistant materials and
equipped with a knurled shaft + dual-screw anti-loosening system for secure.
long-term performance.
Drone Carbon Fiber Propeller
Propeller
The propeller adopts carbon fiber molding process.
Automotive Grade Connectors
Vibration-Resistant Automotive Connectors
Constructed from automotive-grade materials,
both high- and low-voltage connectors incorporate fool-proof alignment,
poor-contact prevention, and superior vibration resistance
for rock-solid system connectivityand extended service life.
High-Specification Materials
With High Reliability
P65m Drone Electric Speed Controller (Esc)
High-Temperature ESC with Automotive Components
The Electric Speed Controller (ESC) uses premium automotive-grade
components designed for elevated temperature resistance.
P65m Powerful Drone Motor
High-Reliability Motor Design
Built with high-temperature resistant materials and
equipped with a knurled shaft + dual-screw anti-loosening system for secure.
long-term performance.
Drone Carbon Fiber Propeller
Propeller
The propeller adopts carbon fiber molding process.
Automotive Grade Connectors
Vibration-Resistant Automotive Connectors
Constructed from automotive-grade materials,
both high- and low-voltage connectors incorporate fool-proof alignment,
poor-contact prevention, and superior vibration resistance
for rock-solid system connectivityand 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
Compatible with most mainstream flight controllers, delivering real-time
data exchange and ongoing monitoring ofessential parameters:
(RPM,throttle position, current, voltage, and temperature.)
The resultis rapid analytics, swift corrective action.
and substantiallyelevated fight safety.
Hobbywing P65m Powerful Drone Motor
Sensor-Driven Redundancy
for Superior Safety

Direct RPM acquisition using a physical sensor for precise,
dependable motor control.

RPM signal intelligently calculated through software algorithms,
eliminating the need for a physical sensor.

2000V-Rated High-Voltage Insulation
Extensively validated with over
1000 hours of aging testing,
guaranteeing maintenance-free
reliability for the entire service life.
Hobbywing P65m Powerful Drone Motor
The motors, ESCs, and propellers are independently
developed and designed by HOBBYWING,
ensuring meticulous attention to every detail
Drone Electric Motor With Propeller
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.

Black Box Data Recording
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.

Big Drone Motor
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.

Support Real-Time Detection And
Feedback of Coil Temperature

Monitor the temperature rise data during motor operation in real time

and take timely countermeasures to ensure flight safety.

Parameter Tuning
Parameter Tuning
P65M - MSC 64×20 Overload Curve
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.
P65M - MSC 72x25 Overload Curve
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.
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.
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P65M ESC CAD
P65M Motor 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.
P65M LED Outline CAD
MSC 72x25 CAD
Product NameP65M Propulsion System
All-in-one thrust system specification
  • Model
  • Max Thrust
  • Recommended takeoff weight per axis
  • Efficiency of recommended takeoff weight
  • Input voltage*
  • Rated voltage
  • Lithium compatible
  • Tube outer diameter
  • Weight(with cable and 72inch Prop)
  • Cable specification
  • Operating temperature
  • Ingress Protection
  • Rated power input
  • Rated power output
  • P65M
  • 138 kg
  • 65kg
  • 7.4g/W / 6.3g/W
  • 280~450 V
  • 335 V
  • 96~107S(LiPo)
  • Φ60mm
  • 7450 g* / 7180 g*
  • Power cable:10AWG 400 mm* Signal cable:800 mm*
  • -35~55℃
  • IP35
  • 10.3 kW
  • 8.8 kW
ESC specification
  • Rated voltage
  • Communication protocol
  • ESC size
  • Weight(with cable)
  • Peak current (3 seconds)
  • Continuous current
  • Ingress Protection
  • Throttle Source
  • Operating pulse width(Nonsupport calibration)
  • Black box
  • 335 V
  • UAVCAN / RS485
  • 225.6*98*60 mm(With plug)
  • 1200 g*
  • 100A
  • 40A
  • IP67
  • CAN+RS485 / CAN+PWM / RS485+PWM
  • 1100~1940 μs
  • 2~48h log
Motor specification
  • KV
  • Slot& Pole
  • Motor size
  • Stator size
  • Ingress Protection
  • Weight(with cable)
  • 9.5KV / 11KV
  • 36N 42P
  • Φ167.1*H110.5 mm
  • Φ156*H45 mm
  • IPX5
  • 5115 g*
Propeller specification
  • Model
  • Weight
  • Material of propeller
  • Mounting dimensions
  • MSC 72x25 / MSC 64x20
  • 1150 g* / 870 g*
  • Carbon fiber composite material
  • D60-6*M6, centre hole D20
P65M-9.5KV & MSC 72×25 Load performance parameters
P65M-9.5KV & MSC 72×25 Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

335V

MSC 72x25

33%

30509

8.9

2977.0

1124

10.2

20.70

2436.1

90.6℃

35%

34417 

10.5 

3507.5 

1194 

9.8 

23.33 

2917.0 

37%

38496 

12.3 

4104.4 

1262 

9.4 

26.09 

3448.1 

39%

42717 

14.2 

4761.5 

1328 

9.0 

28.96 

4027.0 

42%

49254 

17.5 

5846.3 

1424 

8.4 

33.41 

4981.4 

45%

55964 

21.0 

7034.1 

1515 

8.0 

37.98 

6025.0 

49%

65058 

26.1 

8755.8 

1630 

7.4 

44.19 

7542.6 

51%

69627 

28.9 

9670.6 

1685 

7.2 

47.33 

8350.0 

54%

76464 

33.2 

11106.8 

1765 

6.9 

52.04 

9618.1 

57%

83239 

37.7 

12617.1 

1840 

6.6 

56.76 

10935.1 

60%

89906 

42.4 

14196.4 

1911 

6.3 

61.44 

12295.3 

63%

96424 

47.3 

15835.4 

1977 

6.1 

66.08 

13678.7 

66%

102751 

52.3 

17518.4 

2038 

5.9 

70.61 

15068.4 

69%

108843 

57.4 

19222.2 

2094 

5.7 

75.00 

16444.2 

72%

114651 

62.4 

20916.0 

2145 

5.5 

79.17 

17782.8 

75%

120124 

67.4 

22562.7 

2191 

5.3 

83.07 

19059.1 

78%

125200 

72.0 

24120.4 

2232 

5.2 

86.63 

20246.6 

81%

129809 

76.3 

25546.1 

2267 

5.1 

89.77 

21310.4 

84%

133869 

80.0 

26798.1 

2297 

5.0 

92.45 

22235.8 

87%

137287 

83.1 

27838.9 

2323 

4.9 

94.61 

23013.2 

100%

138264 

84.0 

28133.1 

2330 

4.9 

95.21 

23229.1 

The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input. The motor temperature is measured after running for 10 minutes at rated thrust, for reference only.
P65M-9.5KV & MSC 72×25 Load performance parameters
P65M-9.5KV & MSC 72×25 Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

400V

MSC 72x25

33%

30231

7.5

2980.8

1124

10.1

20.51

2414.2

91.2℃

35%

34184 

8.8 

3505.3 

1194 

9.8 

23.08 

2885.5 

37%

38305 

10.3 

4107.8 

1263 

9.3 

25.85 

3418.4 

39%

42560 

11.9 

4778.0 

1329 

8.9 

28.77 

4003.4 

42%

49129 

14.7 

5888.8 

1425 

8.3 

33.33 

4974.0 

45%

55849 

17.8 

7100.7 

1516 

7.9 

38.01 

6034.5 

48%

62655 

21.0 

8393.5 

1602 

7.5 

42.72 

7166.1 

51%

69493 

24.4 

9756.8 

1685 

7.1 

47.40 

8363.9 

54%

76320 

28.0 

11187.9 

1764 

6.8 

52.05 

9614.8 

57%

83097 

31.7 

12688.4 

1839 

6.5 

56.67 

10913.0 

60%

89788 

35.7 

14260.2 

1909 

6.3 

61.27 

12247.4 

63%

96354 

39.8 

15901.2 

1976 

6.1 

65.85 

13624.7 

66%

102750 

44.0 

17601.4 

2037 

5.8 

70.39 

15014.4 

69%

108922 

48.3 

19339.6 

2093 

5.6 

74.85 

16405.1 

72%

114801 

52.7 

21081.6 

2143 

5.4 

79.16 

17763.1 

75%

120302 

56.9 

22779.0 

2189 

5.3 

83.20 

19071.0 

78%

125316 

60.9 

24372.0 

2228 

5.1 

86.86 

20263.4 

81%

129712 

64.5 

25791.9 

2262 

5.0 

89.99 

21315.2 

84%

133328 

67.4 

26966.4 

2289 

4.9 

92.49 

22167.8 

87%

135969 

69.6 

27822.4 

2309 

4.9 

94.24 

22786.0 

100%

136594 

70.1 

28024.2 

2314 

4.9 

94.65 

22933.6 

The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input. The motor temperature is measured after running for 10 minutes at rated thrust, for reference only.
P65M-11KV & MSC 64×20 Load performance parameters
P65M-11KV & MSC 64×20Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

335V

MSC 64x20

33%

27303

9.0

3024.5

1311

9.0

17.56

2410.0

92.6℃

35%

31203 

10.8 

3609.1 

1399 

8.6 

20.05 

2937.5 

37%

35193 

12.7 

4262.5 

1484 

8.3 

22.64 

3518.2 

39%

39272 

14.9 

4978.9 

1567 

7.9 

25.31 

4152.5 

42%

45543 

18.4 

6159.3 

1686 

7.4 

29.42 

5194.6 

45%

51975 

22.2 

7452.1 

1799 

7.0 

33.64 

6337.4 

48%

58531 

26.4 

8844.2 

1906 

6.6 

37.93 

7570.0 

51%

65163 

30.8 

10326.5 

2008 

6.3 

42.26 

8885.6 

54%

71817 

35.5 

11893.1 

2105 

6.0 

46.62 

10274.9 

57%

78436 

40.4 

13538.8 

2196 

5.8 

50.98 

11722.6 

60%

84957 

45.5 

15256.5 

2282 

5.6 

55.33 

13222.0 

63%

91314 

50.8 

17034.5 

2363 

5.4 

59.65 

14758.7 

66%

97443 

56.3 

18853.9 

2437 

5.2 

63.88 

16300.6 

69%

103282 

61.8 

20687.8 

2507 

5.0 

67.97 

17843.7 

72%

108772 

67.2 

22502.2 

2570 

4.8 

71.86 

19339.5 

75%

113858 

72.4 

24258.7 

2627 

4.7 

75.49 

20764.7 

78%

118495 

77.4 

25918.0 

2677 

4.6 

78.78 

22082.1 

81%

122645 

81.9 

27443.6 

2721 

4.5 

81.69 

23274.0 

84%

126281 

86.0 

28806.0 

2759 

4.4 

84.18 

24321.1 

87%

129390 

89.5 

29984.6 

2791 

4.3 

86.27 

25211.8 

90%

131973 

92.4 

30969.6 

2816 

4.3 

87.95 

25932.8 

100%

135161 

96.1 

32188.0 

2848 

4.2 

89.94 

26821.9 

The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input. The motor temperature is measured after running for 10 minutes at rated thrust, for reference only.
P65M-11KV & MSC 64×20 Load performance parameters
P65M-11KV & MSC 64×20 Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

400V

MSC 64x20

33%

27109

7.6

3031.6

1312

8.9

17.41

2392.0

92.8℃

35%

31142 

9.0 

3609.0 

1399 

8.6 

19.98 

2927.1 

37%

35131 

10.7 

4270.4 

1483 

8.2 

22.59 

3507.2 

39%

39130 

12.5 

4999.2 

1565 

7.8 

25.23 

4134.4 

42%

45227 

15.5 

6196.0 

1685 

7.3 

29.28 

5165.9 

45%

51505 

18.7 

7496.2 

1799 

6.9 

33.43 

6297.4 

48%

57983 

22.2 

8884.4 

1907 

6.5 

37.67 

7522.8 

51%

64635 

25.9 

10353.8 

2009 

6.2 

41.99 

8833.5 

54%

71399 

29.8 

11906.5 

2105 

6.0 

46.37 

10219.7 

57%

78182 

33.9 

13549.7 

2196 

5.8 

50.78 

11675.9 

60%

84876 

38.2 

15287.0 

2281 

5.6 

55.20 

13183.3 

63%

91365 

42.8 

17108.5 

2363 

5.3 

59.57 

14740.9 

66%

97534 

47.5 

18983.3 

2439 

5.1 

63.84 

16304.9 

69%

103278 

52.1 

20859.9 

2511 

5.0 

67.91 

17854.6 

72%

108515 

56.7 

22674.3 

2576 

4.8 

71.67 

19331.2 

75%

113190 

60.9 

24364.4 

2632 

4.6 

75.04 

20682.3 

78%

117291 

64.7 

25885.4 

2681 

4.5 

77.99 

21895.3 

81%

120853 

68.1 

27220.9 

2721 

4.4 

80.52 

22941.7 

84%

123973 

71.0 

28387.8 

2754 

4.4 

82.68 

23843.6 

87%

126813 

73.6 

29436.8 

2781 

4.3 

84.59 

24633.7 

90%

129615 

76.1 

30448.0 

2805 

4.3 

86.41 

25378.7 

100%

135144 

80.8 

32321.4 

2843 

4.2 

89.69 

26699.6 

The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input. The motor temperature is measured after running for 10 minutes at rated thrust, for reference only.
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FAQ

P65M
P65m Integrated Propulsion System
P65M
Propulsion System
Elevated to Passenger
Car Standards
Modular Design
Software
Adopts a rigorous modular design.
High Voltage Drone Propulsion System
Fully Isolated Architecture with Protective Earthing
High-voltage power circuits, low-voltage signal circuits,
and protective earthing (PE) are completelyisolated,
delivering reliable data transmission,
stable system performance,
and superior safety for operators and equipment alike.
Dual Redundancy for
Position Sensor

Real-time RPM acquisition via dual channels,

engineered to meet current airworthiness certification standards

while preparing for future regulatory evolution.

Hobbywing P65m Powerful Drone Motor
High-Specification Materials
With High Reliability
P65m Drone Electric Speed Controller (Esc)
High-Temperature ESC with Automotive Components
The Electric Speed Controller (ESC) uses premium automotive-grade
components designed for elevated temperature resistance.
P65m Powerful Drone Motor
High-Reliability Motor Design
Built with high-temperature resistant materials and
equipped with a knurled shaft + dual-screw anti-loosening system for secure.
long-term performance.
Drone Carbon Fiber Propeller
Propeller
The propeller adopts carbon fiber molding process.
Automotive Grade Connectors
Vibration-Resistant Automotive Connectors
Constructed from automotive-grade materials,
both high- and low-voltage connectors incorporate fool-proof alignment,
poor-contact prevention, and superior vibration resistance
for rock-solid system connectivityand extended service life.
High-Specification Materials
With High Reliability
P65m Drone Electric Speed Controller (Esc)
High-Temperature ESC with Automotive Components
The Electric Speed Controller (ESC) uses premium automotive-grade
components designed for elevated temperature resistance.
P65m Powerful Drone Motor
High-Reliability Motor Design
Built with high-temperature resistant materials and
equipped with a knurled shaft + dual-screw anti-loosening system for secure.
long-term performance.
Drone Carbon Fiber Propeller
Propeller
The propeller adopts carbon fiber molding process.
Automotive Grade Connectors
Vibration-Resistant Automotive Connectors
Constructed from automotive-grade materials,
both high- and low-voltage connectors incorporate fool-proof alignment,
poor-contact prevention, and superior vibration resistance
for rock-solid system connectivityand 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
Compatible with most mainstream flight controllers, delivering real-time
data exchange and ongoing monitoring ofessential parameters:
(RPM,throttle position, current, voltage, and temperature.)
The resultis rapid analytics, swift corrective action.
and substantiallyelevated fight safety.
Hobbywing P65m Powerful Drone Motor
Sensor-Driven Redundancy
for Superior Safety

Direct RPM acquisition using a physical sensor for precise,
dependable motor control.

RPM signal intelligently calculated through software algorithms,
eliminating the need for a physical sensor.

2000V-Rated High-Voltage Insulation
Extensively validated with over
1000 hours of aging testing,
guaranteeing maintenance-free
reliability for the entire service life.
Hobbywing P65m Powerful Drone Motor
The motors, ESCs, and propellers are independently
developed and designed by HOBBYWING,
ensuring meticulous attention to every detail
Drone Electric Motor With Propeller
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.

Black Box Data Recording
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.

Big Drone Motor
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.

Support Real-Time Detection And
Feedback of Coil Temperature

Monitor the temperature rise data during motor operation in real time

and take timely countermeasures to ensure flight safety.

Parameter Tuning
Parameter Tuning
P65M - MSC 64×20 Overload Curve
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.
P65M - MSC 72x25 Overload Curve
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.
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.
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HOBBYWING Team
P65M ESC CAD
P65M Motor 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.
P65M LED Outline CAD
MSC 72x25 CAD
Product NameP65M Propulsion System
All-in-one thrust system specification
  • Model
  • Max Thrust
  • Recommended takeoff weight per axis
  • Efficiency of recommended takeoff weight
  • Input voltage*
  • Rated voltage
  • Lithium compatible
  • Tube outer diameter
  • Weight(with cable and 72inch Prop)
  • Cable specification
  • Operating temperature
  • Ingress Protection
  • Rated power input
  • Rated power output
  • P65M
  • 138 kg
  • 65kg
  • 7.4g/W / 6.3g/W
  • 280~450 V
  • 335 V
  • 96~107S(LiPo)
  • Φ60mm
  • 7450 g* / 7180 g*
  • Power cable:10AWG 400 mm* Signal cable:800 mm*
  • -35~55℃
  • IP35
  • 10.3 kW
  • 8.8 kW
ESC specification
  • Rated voltage
  • Communication protocol
  • ESC size
  • Weight(with cable)
  • Peak current (3 seconds)
  • Continuous current
  • Ingress Protection
  • Throttle Source
  • Operating pulse width(Nonsupport calibration)
  • Black box
  • 335 V
  • UAVCAN / RS485
  • 225.6*98*60 mm(With plug)
  • 1200 g*
  • 100A
  • 40A
  • IP67
  • CAN+RS485 / CAN+PWM / RS485+PWM
  • 1100~1940 μs
  • 2~48h log
Motor specification
  • KV
  • Slot& Pole
  • Motor size
  • Stator size
  • Ingress Protection
  • Weight(with cable)
  • 9.5KV / 11KV
  • 36N 42P
  • Φ167.1*H110.5 mm
  • Φ156*H45 mm
  • IPX5
  • 5115 g*
Propeller specification
  • Model
  • Weight
  • Material of propeller
  • Mounting dimensions
  • MSC 72x25 / MSC 64x20
  • 1150 g* / 870 g*
  • Carbon fiber composite material
  • D60-6*M6, centre hole D20
P65M-9.5KV & MSC 72×25 Load performance parameters
P65M-9.5KV & MSC 72×25 Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

335V

MSC 72x25

33%

30509

8.9

2977.0

1124

10.2

20.70

2436.1

90.6℃

35%

34417 

10.5 

3507.5 

1194 

9.8 

23.33 

2917.0 

37%

38496 

12.3 

4104.4 

1262 

9.4 

26.09 

3448.1 

39%

42717 

14.2 

4761.5 

1328 

9.0 

28.96 

4027.0 

42%

49254 

17.5 

5846.3 

1424 

8.4 

33.41 

4981.4 

45%

55964 

21.0 

7034.1 

1515 

8.0 

37.98 

6025.0 

49%

65058 

26.1 

8755.8 

1630 

7.4 

44.19 

7542.6 

51%

69627 

28.9 

9670.6 

1685 

7.2 

47.33 

8350.0 

54%

76464 

33.2 

11106.8 

1765 

6.9 

52.04 

9618.1 

57%

83239 

37.7 

12617.1 

1840 

6.6 

56.76 

10935.1 

60%

89906 

42.4 

14196.4 

1911 

6.3 

61.44 

12295.3 

63%

96424 

47.3 

15835.4 

1977 

6.1 

66.08 

13678.7 

66%

102751 

52.3 

17518.4 

2038 

5.9 

70.61 

15068.4 

69%

108843 

57.4 

19222.2 

2094 

5.7 

75.00 

16444.2 

72%

114651 

62.4 

20916.0 

2145 

5.5 

79.17 

17782.8 

75%

120124 

67.4 

22562.7 

2191 

5.3 

83.07 

19059.1 

78%

125200 

72.0 

24120.4 

2232 

5.2 

86.63 

20246.6 

81%

129809 

76.3 

25546.1 

2267 

5.1 

89.77 

21310.4 

84%

133869 

80.0 

26798.1 

2297 

5.0 

92.45 

22235.8 

87%

137287 

83.1 

27838.9 

2323 

4.9 

94.61 

23013.2 

100%

138264 

84.0 

28133.1 

2330 

4.9 

95.21 

23229.1 

The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input. The motor temperature is measured after running for 10 minutes at rated thrust, for reference only.
P65M-9.5KV & MSC 72×25 Load performance parameters
P65M-9.5KV & MSC 72×25 Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

400V

MSC 72x25

33%

30231

7.5

2980.8

1124

10.1

20.51

2414.2

91.2℃

35%

34184 

8.8 

3505.3 

1194 

9.8 

23.08 

2885.5 

37%

38305 

10.3 

4107.8 

1263 

9.3 

25.85 

3418.4 

39%

42560 

11.9 

4778.0 

1329 

8.9 

28.77 

4003.4 

42%

49129 

14.7 

5888.8 

1425 

8.3 

33.33 

4974.0 

45%

55849 

17.8 

7100.7 

1516 

7.9 

38.01 

6034.5 

48%

62655 

21.0 

8393.5 

1602 

7.5 

42.72 

7166.1 

51%

69493 

24.4 

9756.8 

1685 

7.1 

47.40 

8363.9 

54%

76320 

28.0 

11187.9 

1764 

6.8 

52.05 

9614.8 

57%

83097 

31.7 

12688.4 

1839 

6.5 

56.67 

10913.0 

60%

89788 

35.7 

14260.2 

1909 

6.3 

61.27 

12247.4 

63%

96354 

39.8 

15901.2 

1976 

6.1 

65.85 

13624.7 

66%

102750 

44.0 

17601.4 

2037 

5.8 

70.39 

15014.4 

69%

108922 

48.3 

19339.6 

2093 

5.6 

74.85 

16405.1 

72%

114801 

52.7 

21081.6 

2143 

5.4 

79.16 

17763.1 

75%

120302 

56.9 

22779.0 

2189 

5.3 

83.20 

19071.0 

78%

125316 

60.9 

24372.0 

2228 

5.1 

86.86 

20263.4 

81%

129712 

64.5 

25791.9 

2262 

5.0 

89.99 

21315.2 

84%

133328 

67.4 

26966.4 

2289 

4.9 

92.49 

22167.8 

87%

135969 

69.6 

27822.4 

2309 

4.9 

94.24 

22786.0 

100%

136594 

70.1 

28024.2 

2314 

4.9 

94.65 

22933.6 

The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input. The motor temperature is measured after running for 10 minutes at rated thrust, for reference only.
P65M-11KV & MSC 64×20 Load performance parameters
P65M-11KV & MSC 64×20Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

335V

MSC 64x20

33%

27303

9.0

3024.5

1311

9.0

17.56

2410.0

92.6℃

35%

31203 

10.8 

3609.1 

1399 

8.6 

20.05 

2937.5 

37%

35193 

12.7 

4262.5 

1484 

8.3 

22.64 

3518.2 

39%

39272 

14.9 

4978.9 

1567 

7.9 

25.31 

4152.5 

42%

45543 

18.4 

6159.3 

1686 

7.4 

29.42 

5194.6 

45%

51975 

22.2 

7452.1 

1799 

7.0 

33.64 

6337.4 

48%

58531 

26.4 

8844.2 

1906 

6.6 

37.93 

7570.0 

51%

65163 

30.8 

10326.5 

2008 

6.3 

42.26 

8885.6 

54%

71817 

35.5 

11893.1 

2105 

6.0 

46.62 

10274.9 

57%

78436 

40.4 

13538.8 

2196 

5.8 

50.98 

11722.6 

60%

84957 

45.5 

15256.5 

2282 

5.6 

55.33 

13222.0 

63%

91314 

50.8 

17034.5 

2363 

5.4 

59.65 

14758.7 

66%

97443 

56.3 

18853.9 

2437 

5.2 

63.88 

16300.6 

69%

103282 

61.8 

20687.8 

2507 

5.0 

67.97 

17843.7 

72%

108772 

67.2 

22502.2 

2570 

4.8 

71.86 

19339.5 

75%

113858 

72.4 

24258.7 

2627 

4.7 

75.49 

20764.7 

78%

118495 

77.4 

25918.0 

2677 

4.6 

78.78 

22082.1 

81%

122645 

81.9 

27443.6 

2721 

4.5 

81.69 

23274.0 

84%

126281 

86.0 

28806.0 

2759 

4.4 

84.18 

24321.1 

87%

129390 

89.5 

29984.6 

2791 

4.3 

86.27 

25211.8 

90%

131973 

92.4 

30969.6 

2816 

4.3 

87.95 

25932.8 

100%

135161 

96.1 

32188.0 

2848 

4.2 

89.94 

26821.9 

The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input. The motor temperature is measured after running for 10 minutes at rated thrust, for reference only.
P65M-11KV & MSC 64×20 Load performance parameters
P65M-11KV & MSC 64×20 Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

400V

MSC 64x20

33%

27109

7.6

3031.6

1312

8.9

17.41

2392.0

92.8℃

35%

31142 

9.0 

3609.0 

1399 

8.6 

19.98 

2927.1 

37%

35131 

10.7 

4270.4 

1483 

8.2 

22.59 

3507.2 

39%

39130 

12.5 

4999.2 

1565 

7.8 

25.23 

4134.4 

42%

45227 

15.5 

6196.0 

1685 

7.3 

29.28 

5165.9 

45%

51505 

18.7 

7496.2 

1799 

6.9 

33.43 

6297.4 

48%

57983 

22.2 

8884.4 

1907 

6.5 

37.67 

7522.8 

51%

64635 

25.9 

10353.8 

2009 

6.2 

41.99 

8833.5 

54%

71399 

29.8 

11906.5 

2105 

6.0 

46.37 

10219.7 

57%

78182 

33.9 

13549.7 

2196 

5.8 

50.78 

11675.9 

60%

84876 

38.2 

15287.0 

2281 

5.6 

55.20 

13183.3 

63%

91365 

42.8 

17108.5 

2363 

5.3 

59.57 

14740.9 

66%

97534 

47.5 

18983.3 

2439 

5.1 

63.84 

16304.9 

69%

103278 

52.1 

20859.9 

2511 

5.0 

67.91 

17854.6 

72%

108515 

56.7 

22674.3 

2576 

4.8 

71.67 

19331.2 

75%

113190 

60.9 

24364.4 

2632 

4.6 

75.04 

20682.3 

78%

117291 

64.7 

25885.4 

2681 

4.5 

77.99 

21895.3 

81%

120853 

68.1 

27220.9 

2721 

4.4 

80.52 

22941.7 

84%

123973 

71.0 

28387.8 

2754 

4.4 

82.68 

23843.6 

87%

126813 

73.6 

29436.8 

2781 

4.3 

84.59 

24633.7 

90%

129615 

76.1 

30448.0 

2805 

4.3 

86.41 

25378.7 

100%

135144 

80.8 

32321.4 

2843 

4.2 

89.69 

26699.6 

The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input. The motor temperature is measured after running for 10 minutes at rated thrust, for reference only.
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