P65M - Integrated Propulsion System for Industrial Drones
P65m Integrated Propulsion System
P65M
Integrated 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 Integrated 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
  • 130kg (5s)
  • 65kg
  • 6.3g/W / 5.4g/W
  • 280~450V DC
  • 335V
  • 96~107S(LiPo)
  • Φ60mm
  • 7465±60g / 7185g±60g
  • Power cord: 10AWG*400mm Signal line: 800mm
  • -35~55℃
  • IP35
  • 10.4 KW
  • 8.6 KW
*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
All the above data were obtained under conditions of adequate air cooling for both the ESC and the motor. This product requires proper air cooling for both the ESC and the motor; therefore, an appropriate mounting location must be considered during the overall system design.
ESC specification
  • Model
  • Communication protocol
  • ESC size
  • Weight(with cable)
  • Peak current (3 seconds)
  • Continuous current
  • ESC Rated power output
  • Ingress Protection
  • Double throttle signal
  • Operating pulse width(Nonsupport calibration)
  • Black box
  • 100A-FOC
  • UAVCAN / RS485
  • 225.6*98*60 mm(With plug)
  • 1200±20g
  • 100A(3s)
  • 40A
  • 14KW
  • IP67
  • CAN+RS485 / CAN+PWM / RS485+PWM
  • 1100~1940 μs
  • 2~48h log
Motor specification
  • Model
  • KV
  • Motor diameter
  • Slot& Pole
  • Ingress Protection
  • Weight(with cable)
  • Motor temperature signal
  • Motor position sensor signal
  • 15645
  • 9.5KV / 11KV
  • 167.1*H110.5mm
  • 36N 42P
  • IPX5
  • 5115g±50
  • Standard configuration
  • Standard configuration
Propeller specification
  • Model
  • Weight
  • Material of Props
  • Mounting dimensions
  • MSC 72x25 / MSC 64x20
  • 1150±20g / 870±20g
  • Carbon unfolding Props
  • D60-6*M6, centre hole D20
MSC 72x25-9.5KV Load performance parameters
MSC 72x25-9.5KV Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Output Power(W)

Temperature(℃)

335V

MSC 72x25

33%

27976

9.7

3252.3

1133

8.6

20.33

2412.3

90.6℃

35%

31520

11.3

3801.2

1204

8.3

23.02

2900.8

37%

35181

13.1

4399.1

1272

8.0

25.79

3434.3

39%

38943

15.1

5044.7

1338

7.7

28.62

4010.3

42%

44736

18.2

6098.7

1433

7.3

32.97

4947.9

45%

50665

21.6

7248.6

1524

7.0

37.39

5965.7

48%

56679

25.3

8485.7

1610

6.7

41.84

7055.2

51%

62728

29.2

9800.2

1692

6.4

46.31

8207.9

54%

68768

33.4

11181.7

1771

6.2

50.79

9415.4

57%

74754

37.7

12619.4

1844

5.9

55.24

10668.2

60%

80641

42.1

14102.1

1914

5.7

59.66

11955.4

63%

86388

46.6

15617.9

1979

5.5

64.01

13264.4

66%

91953

51.2

17154.0

2039

5.4

68.28

14580.4

69%

97295

55.8

18696.2

2095

5.2

72.41

15886.9

72%

102373

60.4

20228.4

2147

5.1

76.37

17166.1

75%

107144

64.9

21732.1

2194

4.9

80.10

18399.3

78%

111568

69.2

23186.0

2237

4.8

83.55

19567.4

81%

115601

73.3

24565.7

2275

4.7

86.67

20651.5

84%

119200

77.1

25843.6

2310

4.6

89.42

21632.9

87%

122318

80.6

26989.1

2341

4.5

91.76

22493.3

90%

124909

83.5

27969.4

2367

4.5

93.67

23214.7

100%

129081

88.4

29606.0

2410

4.4

96.65

24387.8

The above 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 mins, which is for reference only.
MSC 72x25-9.5KV Load performance parameters
MSC 72x25-9.5KV 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

MSC 72x25

33%

27898

8.7

3492.2

1132

8.0

22.06

2420.3

91.2℃

35%

31399

10.1

4034.1

1202

7.8

22.99

2892.8

37%

35063

11.6

4636.6

1271

7.6

25.71

3420.0

39%

38856

13.2

5294.5

1338

7.3

28.54

3997.4

42%

44722

15.9

6372.8

1434

7.0

32.93

4945.8

45%

50726

18.9

7545.3

1526

6.7

37.42

5977.3

48%

56800

22.0

8796.8

1612

6.5

41.92

7076.6

51%

62889

25.3

10115.8

1694

6.2

46.41

8231.7

54%

68950

28.7

11493.6

1771

6.0

50.87

9433.9

57%

74947

32.3

12924.2

1844

5.8

55.29

10676.6

60%

80851

36.0

14402.2

1913

5.6

59.68

11954.0

63%

86635

39.8

15922.2

1978

5.4

64.03

13259.6

66%

92274

43.7

17476.6

2038

5.3

68.34

14584.7

69%

97740

47.6

19055.0

2095

5.1

72.57

15917.5

72%

102998

51.6

20642.1

2147

5.0

76.68

17241.8

75%

108007

55.5

22217.5

2196

4.9

80.62

18537.1

78%

112717

59.4

23753.9

2241

4.7

84.30

19778.0

81%

117062

63.0

25217.0

2281

4.6

87.65

20935.8

84%

120963

66.4

26565.3

2317

4.6

90.58

21978.4

87%

124319

69.4

27749.8

2348

4.5

93.01

22872.4

90%

127012

71.8

28714.5

2374

4.4

94.89

23583.6

100%

129858

74.3

29746.1

2400

4.4

96.78

24325.0

The above 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 mins, which is for reference only.
MSC 64x20-11KV Load performance parameters
MSC 64x20-11KV 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

MSC 64x20

33%

25658

10.3

3436.8

1320

7.5

17.35

2397.9

92.6℃

35%

29263

12.0

4017.5

1405

7.3

19.82

2917.0

37%

32952

14.0

4685.4

1490

7.0

22.43

3499.9

39%

36723

16.2

5428.5

1573

6.8

25.15

4143.8

42%

42520

19.9

6660.4

1694

6.4

29.39

5214.8

45%

48464

23.9

8006.1

1810

6.1

33.76

6397.3

48%

54527

28.2

9442.9

1919

5.8

38.19

7674.2

51%

60674

32.7

10957.7

2021

5.5

42.67

9030.5

54%

66864

37.4

12545.9

2117

5.3

47.16

10454.5

57%

73053

42.4

14207.7

2206

5.1

51.68

11938.4

60%

79193

47.6

15944.7

2289

5.0

56.22

13476.0

63%

85231

53.0

17754.0

2366

4.8

60.77

15059.7

66%

91114

58.6

19624.3

2439

4.6

65.31

16677.5

69%

96785

64.3

21532.4

2506

4.5

69.77

18309.2

72%

102184

70.0

23442.5

2568

4.4

74.09

19925.3

75%

107253

75.5

25308.6

2625

4.2

78.18

21487.7

78%

111931

80.8

27078.5

2676

4.1

81.92

22953.2

81%

116160

85.6

28699.9

2720

4.0

85.23

24279.0

84%

119880

89.9

30126.3

2758

4.0

88.05

25428.0

87%

123033

93.5

31322.1

2789

3.9

90.32

26374.4

90%

125565

96.3

32263.8

2812

3.9

92.05

27105.6

100%

128912

99.9

33470.1

2841

3.9

94.17

28017.5

The above 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 mins, which is for reference only.
MSC 64x20-11KV Load performance parameters
MSC 64x20-11KV 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

MSC 64x20

33%

25312

9.3

3714.7

1326

6.8

17.55

2437.0

92.8℃

35%

28798

10.8

4314.2

1413

6.7

20.01

2961.1

37%

32374

12.5

4989.8

1499

6.5

22.59

3545.4

39%

36047

14.3

5731.5

1582

6.3

25.28

4187.1

42%

41733

17.4

6947.7

1703

6.0

29.44

5249.1

45%

47618

20.7

8264.4

1818

5.8

33.71

6415.7

48%

53668

24.2

9660.9

1926

5.6

38.03

7669.8

51%

59834

27.9

11125.8

2028

5.4

42.37

8997.2

54%

66057

31.7

12656.4

2123

5.2

46.74

10388.8

57%

72271

35.7

14255.4

2212

5.1

51.12

11839.9

60%

78403

39.9

15924.9

2296

4.9

55.52

13347.2

63%

84380

44.3

17660.3

2375

4.8

59.94

14903.5

66%

90131

48.7

19445.6

2449

4.6

64.32

16492.8

69%

95589

53.3

21251.4

2518

4.5

68.61

18087.8

72%

100696

57.8

23037.3

2581

4.4

72.72

19651.0

75%

105405

62.1

24757.7

2637

4.3

76.55

21139.2

78%

109684

66.2

26369.2

2687

4.2

80.01

22511.4

81%

113518

69.9

27837.6

2729

4.1

83.06

23735.8

84%

116914

73.2

29143.7

2764

4.0

85.67

24796.0

87%

119903

76.1

30285.4

2793

4.0

87.86

25692.2

90%

122543

78.6

31278.0

2816

3.9

89.68

26440.6

100%

130923

85.4

34072.0

2866

3.8

94.11

28245.3

The above 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 mins, which is for reference only.
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Manuals & Documents

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FAQ

P65M
P65m Integrated Propulsion System
P65M
Integrated 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 Integrated 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
  • 130kg (5s)
  • 65kg
  • 6.3g/W / 5.4g/W
  • 280~450V DC
  • 335V
  • 96~107S(LiPo)
  • Φ60mm
  • 7465±60g / 7185g±60g
  • Power cord: 10AWG*400mm Signal line: 800mm
  • -35~55℃
  • IP35
  • 10.4 KW
  • 8.6 KW
*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
All the above data were obtained under conditions of adequate air cooling for both the ESC and the motor. This product requires proper air cooling for both the ESC and the motor; therefore, an appropriate mounting location must be considered during the overall system design.
ESC specification
  • Model
  • Communication protocol
  • ESC size
  • Weight(with cable)
  • Peak current (3 seconds)
  • Continuous current
  • ESC Rated power output
  • Ingress Protection
  • Double throttle signal
  • Operating pulse width(Nonsupport calibration)
  • Black box
  • 100A-FOC
  • UAVCAN / RS485
  • 225.6*98*60 mm(With plug)
  • 1200±20g
  • 100A(3s)
  • 40A
  • 14KW
  • IP67
  • CAN+RS485 / CAN+PWM / RS485+PWM
  • 1100~1940 μs
  • 2~48h log
Motor specification
  • Model
  • KV
  • Motor diameter
  • Slot& Pole
  • Ingress Protection
  • Weight(with cable)
  • Motor temperature signal
  • Motor position sensor signal
  • 15645
  • 9.5KV / 11KV
  • 167.1*H110.5mm
  • 36N 42P
  • IPX5
  • 5115g±50
  • Standard configuration
  • Standard configuration
Propeller specification
  • Model
  • Weight
  • Material of Props
  • Mounting dimensions
  • MSC 72x25 / MSC 64x20
  • 1150±20g / 870±20g
  • Carbon unfolding Props
  • D60-6*M6, centre hole D20
MSC 72x25-9.5KV Load performance parameters
MSC 72x25-9.5KV Load performance parameters

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Output Power(W)

Temperature(℃)

335V

MSC 72x25

33%

27976

9.7

3252.3

1133

8.6

20.33

2412.3

90.6℃

35%

31520

11.3

3801.2

1204

8.3

23.02

2900.8

37%

35181

13.1

4399.1

1272

8.0

25.79

3434.3

39%

38943

15.1

5044.7

1338

7.7

28.62

4010.3

42%

44736

18.2

6098.7

1433

7.3

32.97

4947.9

45%

50665

21.6

7248.6

1524

7.0

37.39

5965.7

48%

56679

25.3

8485.7

1610

6.7

41.84

7055.2

51%

62728

29.2

9800.2

1692

6.4

46.31

8207.9

54%

68768

33.4

11181.7

1771

6.2

50.79

9415.4

57%

74754

37.7

12619.4

1844

5.9

55.24

10668.2

60%

80641

42.1

14102.1

1914

5.7

59.66

11955.4

63%

86388

46.6

15617.9

1979

5.5

64.01

13264.4

66%

91953

51.2

17154.0

2039

5.4

68.28

14580.4

69%

97295

55.8

18696.2

2095

5.2

72.41

15886.9

72%

102373

60.4

20228.4

2147

5.1

76.37

17166.1

75%

107144

64.9

21732.1

2194

4.9

80.10

18399.3

78%

111568

69.2

23186.0

2237

4.8

83.55

19567.4

81%

115601

73.3

24565.7

2275

4.7

86.67

20651.5

84%

119200

77.1

25843.6

2310

4.6

89.42

21632.9

87%

122318

80.6

26989.1

2341

4.5

91.76

22493.3

90%

124909

83.5

27969.4

2367

4.5

93.67

23214.7

100%

129081

88.4

29606.0

2410

4.4

96.65

24387.8

The above 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 mins, which is for reference only.
MSC 72x25-9.5KV Load performance parameters
MSC 72x25-9.5KV 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

MSC 72x25

33%

27898

8.7

3492.2

1132

8.0

22.06

2420.3

91.2℃

35%

31399

10.1

4034.1

1202

7.8

22.99

2892.8

37%

35063

11.6

4636.6

1271

7.6

25.71

3420.0

39%

38856

13.2

5294.5

1338

7.3

28.54

3997.4

42%

44722

15.9

6372.8

1434

7.0

32.93

4945.8

45%

50726

18.9

7545.3

1526

6.7

37.42

5977.3

48%

56800

22.0

8796.8

1612

6.5

41.92

7076.6

51%

62889

25.3

10115.8

1694

6.2

46.41

8231.7

54%

68950

28.7

11493.6

1771

6.0

50.87

9433.9

57%

74947

32.3

12924.2

1844

5.8

55.29

10676.6

60%

80851

36.0

14402.2

1913

5.6

59.68

11954.0

63%

86635

39.8

15922.2

1978

5.4

64.03

13259.6

66%

92274

43.7

17476.6

2038

5.3

68.34

14584.7

69%

97740

47.6

19055.0

2095

5.1

72.57

15917.5

72%

102998

51.6

20642.1

2147

5.0

76.68

17241.8

75%

108007

55.5

22217.5

2196

4.9

80.62

18537.1

78%

112717

59.4

23753.9

2241

4.7

84.30

19778.0

81%

117062

63.0

25217.0

2281

4.6

87.65

20935.8

84%

120963

66.4

26565.3

2317

4.6

90.58

21978.4

87%

124319

69.4

27749.8

2348

4.5

93.01

22872.4

90%

127012

71.8

28714.5

2374

4.4

94.89

23583.6

100%

129858

74.3

29746.1

2400

4.4

96.78

24325.0

The above 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 mins, which is for reference only.
MSC 64x20-11KV Load performance parameters
MSC 64x20-11KV 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

MSC 64x20

33%

25658

10.3

3436.8

1320

7.5

17.35

2397.9

92.6℃

35%

29263

12.0

4017.5

1405

7.3

19.82

2917.0

37%

32952

14.0

4685.4

1490

7.0

22.43

3499.9

39%

36723

16.2

5428.5

1573

6.8

25.15

4143.8

42%

42520

19.9

6660.4

1694

6.4

29.39

5214.8

45%

48464

23.9

8006.1

1810

6.1

33.76

6397.3

48%

54527

28.2

9442.9

1919

5.8

38.19

7674.2

51%

60674

32.7

10957.7

2021

5.5

42.67

9030.5

54%

66864

37.4

12545.9

2117

5.3

47.16

10454.5

57%

73053

42.4

14207.7

2206

5.1

51.68

11938.4

60%

79193

47.6

15944.7

2289

5.0

56.22

13476.0

63%

85231

53.0

17754.0

2366

4.8

60.77

15059.7

66%

91114

58.6

19624.3

2439

4.6

65.31

16677.5

69%

96785

64.3

21532.4

2506

4.5

69.77

18309.2

72%

102184

70.0

23442.5

2568

4.4

74.09

19925.3

75%

107253

75.5

25308.6

2625

4.2

78.18

21487.7

78%

111931

80.8

27078.5

2676

4.1

81.92

22953.2

81%

116160

85.6

28699.9

2720

4.0

85.23

24279.0

84%

119880

89.9

30126.3

2758

4.0

88.05

25428.0

87%

123033

93.5

31322.1

2789

3.9

90.32

26374.4

90%

125565

96.3

32263.8

2812

3.9

92.05

27105.6

100%

128912

99.9

33470.1

2841

3.9

94.17

28017.5

The above 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 mins, which is for reference only.
MSC 64x20-11KV Load performance parameters
MSC 64x20-11KV 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

MSC 64x20

33%

25312

9.3

3714.7

1326

6.8

17.55

2437.0

92.8℃

35%

28798

10.8

4314.2

1413

6.7

20.01

2961.1

37%

32374

12.5

4989.8

1499

6.5

22.59

3545.4

39%

36047

14.3

5731.5

1582

6.3

25.28

4187.1

42%

41733

17.4

6947.7

1703

6.0

29.44

5249.1

45%

47618

20.7

8264.4

1818

5.8

33.71

6415.7

48%

53668

24.2

9660.9

1926

5.6

38.03

7669.8

51%

59834

27.9

11125.8

2028

5.4

42.37

8997.2

54%

66057

31.7

12656.4

2123

5.2

46.74

10388.8

57%

72271

35.7

14255.4

2212

5.1

51.12

11839.9

60%

78403

39.9

15924.9

2296

4.9

55.52

13347.2

63%

84380

44.3

17660.3

2375

4.8

59.94

14903.5

66%

90131

48.7

19445.6

2449

4.6

64.32

16492.8

69%

95589

53.3

21251.4

2518

4.5

68.61

18087.8

72%

100696

57.8

23037.3

2581

4.4

72.72

19651.0

75%

105405

62.1

24757.7

2637

4.3

76.55

21139.2

78%

109684

66.2

26369.2

2687

4.2

80.01

22511.4

81%

113518

69.9

27837.6

2729

4.1

83.06

23735.8

84%

116914

73.2

29143.7

2764

4.0

85.67

24796.0

87%

119903

76.1

30285.4

2793

4.0

87.86

25692.2

90%

122543

78.6

31278.0

2816

3.9

89.68

26440.6

100%

130923

85.4

34072.0

2866

3.8

94.11

28245.3

The above 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 mins, which is for reference only.
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