P115M - High Voltage Integrated Drone Propulsion System
Hobbywing P115 Drone Propulsion System
P115M
The Industry's First 800V Coaxial Integrated Propulsion System
Specially designed for firefighting tethered drones and heavy-lift cargo eVTOLs.
Max. input voltag850V DC
Max. thrust240kg
Highly Integrated
Innovative Design
Hobbywing P115 Drone Motor With Propeller
At 800V and over 100kg-class thrust, the motor, ESC, and propeller are fully integrated in a groundbreaking design that
eliminates exposed cables. This streamlines the entire wiring layout, drastically reduces installation complexity and
maintenance costs, and eliminates failures from cable tension, abrasion, or short circuits at the source.
Significantly Enhancing Overall System Reliability.
Ultra Short Wiring
Shortened Three-Phase Cables minimizes transmission losses and EMI from long runs.
Delivering Higher System Efficiency, Superior Stability, and Cleaner power Performance.
All wiring placed inside durable carbon tubes to resist aging, moisture ingress, salt spray corrosion, and dust.
Ensuring extended, maintenance-free lifespan in demanding applications.
Internal Support Design For Tube Clamp Holders
The patented internal support structure effectively suppresses vibration and displacement of
arms under heavy-lift conditions, ensuring continuous, stable, and reliable propulsion output.
Compatible with arm thicknesses ranging from 2 mm to 5 mm, accommodating a wide variety
of materials and manufacturing processes for maximum integration flexibility.
  • Highly integrated design
  • Ultra-short wiring
  • All built-in connections
  • Innovative patented internal support design for tube clip holder
Highly Integrated
Innovative Design
Hobbywing P115 Drone Motor With Propeller
Highly integrated design
At 800V and over 100kg-class thrust, the motor, ESC, and propeller are fully integrated in a groundbreaking design that eliminates exposed cables. This streamlines the entire wiring layout, drastically reduces installation complexity and maintenance costs, and eliminates failures from cable tension, abrasion, or short circuits at the source. Significantly Enhancing Overall System Reliability.
Ultra Short Wiring
Ultra-short wiring
Shortened Three-Phase Cables minimizes transmission losses and EMI from long runs. Delivering Higher System Efficiency, Superior Stability, and Cleaner power Performance.
All Built In Connections
All built-in connections
All wiring placed inside durable carbon tubes to resist aging, moisture ingress, salt spray corrosion, and dust. Ensuring extended, maintenance-free lifespan in demanding applications.
Internal Support Design For Tube Clamp Holders
Innovative patented internal support design for tube clip holder
The patented internal support structure effectively suppresses vibration and displacement of arms under heavy-lift conditions, ensuring continuous, stable, and reliable propulsion output. Compatible with arm thicknesses ranging from 2 mm to 5 mm, accommodating a wide variety of materials and manufacturing processes for maximum integration flexibility.
800V High-Voltage SiC Platform
Efficient Energy-Saving
Supports 810v Dc Input
Supports 850V DC input, reaching the top
industrial standard.
At the same power level, transmission current is significantly reduced, minimizing energy losses, allowing thinner and lighter cables, and substantially increasing overall power density.
Automotive Sic Mosfets
Equipped with cutting-edge third-generation automotive-grade SiC MOSFETs, the system achieves ultra-low switching losses and a substantial boost in overall efficiency. Ideal for demanding, mission-critical applications such as firefighting, cargo transport, and heavy-lift industrial operations.
Broad Compatibility &
Flexible Adaptation

Compatible with D60 and D80 arm mount methods,

the product supports both flat and coaxial layouts,

and offers 64-inch and 73-inch quick-release carbon fiber propellers,

meeting the overall size requirements.

P115 Drone Motor With Carbon Fiber Propeller
Robust Protection,
Ready for Harsh Environments

The motor features high-temperature resistant enameled wires rated up to 200°C, an IPX5

protection rating, and insulation capable of withstanding up to 2,700V. The system’s internal potting

process provides robust protection against high temperatures, humidity, and firefighting powders.

Rated
up to
200℃

Protection rating
IPX5

Withstanding up to
2700V
High Temperature Resistant Enameled WireHigh-temperature
resistant enameled wires
Ipx5 Waterproof Drone Motor
Multiple Redundancy
Designs for a Safer Flight
Control redundancy

The product boasts dual-mode operation with sensorless FOC as the primary

control and sensor FOC as backup for enhanced safety. Two sets of signal channels

can be converted in real time to enhance the reliability of the propulsion system./p>

Real Time Signal Channel Conversion

Communication redundancy

The dual heterogeneous communication links via CAN bus and RS485 are supported.

Speed information is obtained in real time through dual channels to meet airworthiness

certification requirements and flexibly respond to future regulatory requirements.

Motor Supporting Can Bus And Rs485 Communication
Throttle redundancy

Three throttle combination methods are supported

PWM+CAN digital throttle
is the default configuration
PWM+RS485
is optional
CAN+RS485
is optional

Adapts seamlessly to the communication needs of various flight controllers, enabling real-time

upload of critical flight data and continuous monitoring of key parameters.

(RPM, Throttle Position, Current, Voltage, and Temperature)

Hobbywing P65m Powerful Drone Motor
Two types of power distribution schemes

In addition to conventional high‑voltage input, it also supports an

independent high and low voltage power distribution method (with low

voltage at 24V). Both power distribution schemes are fully compatible.

Independent High And Low Voltage Distribution Method
Reliable Design,
Automotive-Grade Materialsn

Automotive-Grade System Design

Modular Design
The software
adopts a rigorous modular design.
High Voltage Drone Propulsion System
The hardware 
system implements a fully isolated architecture, separating high-voltage power circuits, low-voltage signal circuits, and protective earthing (PE). This ensures reliable data transmission, stable equipment operation, and significantly enhanced safety for both personnel and connected systems.
  • Structural
    design
  • High-
    specification
    materials
  • Tilt design
    of the tube
    clip holder
Coaxial Drone Motor
Structural design
The dual-rotor coaxial structure significantly shortens arm length and
enhances effective payload space. In addition, the product features a
sleek and streamlined design with no exposed cables.
Vtol Drone Electric Motor And Esc
High-specification materials
The ESCs feature automotive-grade components, motors are crafted from
high-temperature-resistant materials, propellers are made of carbon fiber materials
with higher reliability, and connectors adopt automotive-grade materials, which are
foolproof, anti-false connection and vibration-resistant, providing reliable system
connection and extended service life.
3° Tube Clamp Holder Tilt Design
Tilt design of the tube clip holder
The 3° tube clip holder tilt design improves coaxial flight control efficiency,
hovering stability, and maneuverability, easily adaptable to various flight controllers.
Multiple Protection Functions
Throttle loss
warning
Reverse polarity
protection
Undervoltage
warning
Overvoltage
warning
Overcurrent
protection
Over-temperature
warning
Motor stall
protection
Motor overspeed
protection
Fail to reset throttle
to zero protection
Fault Storage & Black Box
Black Box Data Recording
The fault storage function
can record fault codes during
operation, making it easier to
accurately trace the cause.
Real-time recording of UAV operation
data within 2-48 hours facilitates
subsequent data analysis.
Fault Storage Function
The black box
captures real-time operational
data with milliseconds, allowing
for traceability and analysis.
Fast Parameter Adjustment
and Firmware OTA Upgrade

With HOBBYWING’s proprietary host computer software, users can adjust drive

parameters, motor rotation direction, and light color (default green) effortlessly based on

application requirements to optimize flight performance and upgrade the latest firmware.

Parameter Adjustment And Firmware Ota Upgrade
P115M & MSC 64×23-P Overload Curve
Test Voltage: 720V

  • *he above data provides the maximum permissible temperature values for each overload point, measured under optimal conditions: effective heat dissipation, an ambient temperature of 25°C, sea-level altitude, and consistent rotational speed.
  • The horizontal axis (time) represents the maximum safe operating duration for each overload point under the stated conditions. Exceeding this duration during actual flight may cause irreversible damage to the propulsion system due to overheating.
  • Please note: To prioritize flight safety, the propulsion system will not automatically shut down. Therefore, strict monitoring is required to avoid overloading beyond the specified time limits.
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
P115M CAD
MSC 64×23-P CAD
MSC 73×21-P CAD
Product Name P115M
  • MSC 64x23-P
  • MSC 73x21-P (Coming soon)
Integrated thrust system specification
  • Model
  • Max Thrust
  • Rated thrust
  • System efficiency
  • Input voltage
  • Rated voltage
  • Tube outer diameter
  • Weight(with cable and Props)
  • Cable specification
  • Operating temperature
  • Ingress protection
  • Rated power input(single motor)
  • Rated power output(single motor)
  • Signal cable define
  • P115M
  • 234 kg
  • 115 kg
  • 5.5 g/W
  • 500~850V
  • 720 V
  • Φ80mm(Wall thickness varies by material, ends require specific holes. See specs.)
  • 19.7 kg ± 50 g
  • Power cable:12AWG*2000 mm Signal cable:2200 mm
  • -35~55 ℃
  • IP35
  • 10608 W
  • 9121 W
  • Blue-CAN-GND、Red-CANH,Brown-CANL、Black-Shielded、Green-PWM、,Gray-PWM-GND、Orange-DC24V+、Yellow-DC24V-
  • P115M
  • 240 kg
  • 115 kg
  • 6.2 g/W
  • 500~850V
  • 720 V
  • Φ80mm(Wall thickness varies by material, ends require specific holes. See specs.)
  • 20.1 kg ±150 g
  • Power cable:12AWG*2000 mm Signal cable:2200 mm
  • -35~55 ℃
  • IP35
  • 9650 W
  • 8400 W
  • Blue-CAN-GND、Red-CANH,Brown-CANL、Black-Shielded、Green-PWM、,Gray-PWM-GND、Orange-DC24V+、Yellow-DC24V-
ESC specification
  • Rated voltage
  • Communication protocol
  • ESC size
  • Weight(with cable)
  • Peak current (10 seconds)
  • Continuous current
  • Ingress Protection
  • Double throttle signal
  • Operating pulse width(Not supported)
  • Black box
  • 720 V
  • CAN(customizable RS485)
  • 211 mm*104 mm*67 mm(Without plug)
  • 1880±50 g
  • 45 A
  • 15 A
  • IP67
  • CAN+RS485 / CAN+PWM / RS485+PWM
  • 1100~1940 μs
  • 2~48h log
  • 720 V
  • CAN(customizable RS485)
  • 211 mm*104 mm*67 mm(Without plug)
  • 1880±50 g
  • 45 A
  • 15 A
  • IP67
  • CAN+RS485 / CAN+PWM / RS485+PWM
  • 1100~1940 μs
  • 2~48h log
Motor specification
  • Stator size
  • KV
  • Motor diameter
  • Slot& Pole
  • Ingress Protection
  • Weight(with cable)
  • 156*50 mm
  • 5.5 KV
  • Φ167.1±0.1 mm
  • 36N42P
  • IPX5
  • 5172 g
  • 156*50 mm
  • 5KV
  • Φ167.1±0.1 mm
  • 36N42P
  • IPX5
  • 5182 g
Propeller specification
  • Model
  • Weight
  • Material of Props
  • Mounting dimensions
  • MSC 64x23-P
  • 1035 g
  • Carbon unfolding Props
  • D60-6*M6, centre hole D20
  • MSC 73x21-P
  • 1254 g
  • Carbon unfolding Props
  • D60-6*M6, centre hole D20
MSC 64x23-P-720V Load Performance Parameters of Upper Rotor of Coaxial
MSC 64x23-P-720V Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Efficiency(%)

Efficiency(g/W)

Power Output(W)

Temperature(℃)

720V

MSC 64x23-P

38%

63370

12.5

9007.2

82.10

7.0

7394.9

/

40%

70510 

14.5 

10440.0 

83.09 

6.8 

8674.6 

42%

77805 

16.6 

11980.8 

83.92 

6.5 

10054.3 

44%

85235 

18.9 

13629.6 

84.60 

6.3 

11530.6 

46%

92777 

21.4 

15372.0 

85.17 

6.0 

13092.3 

48%

100409 

23.9 

17215.2 

85.62 

5.8 

14739.7 

50%

108106 

26.6 

19144.8 

86.00 

5.6 

16464.5 

52%

115840 

29.4 

21153.6 

86.30 

5.5 

18255.6 

54%

123586 

32.3 

23234.4 

86.54 

5.3 

20107.0 

56%

131313 

35.3 

25380.0 

86.74 

5.2 

22014.6 

58%

138994 

38.3 

27576.0 

86.89 

5.0 

23960.8 

60%

146597 

41.4 

29815.2 

87.01 

4.9 

25942.2 

62%

154091 

44.6 

32097.6 

87.08 

4.8 

27950.6 

64%

161446 

47.8 

34416.0 

87.13 

4.7 

29986.7 

66%

168629 

51.0 

36748.8 

87.14 

4.6 

32022.9 

68%

175608 

54.3 

39110.4 

87.11 

4.5 

34069.1 

70%

182351 

57.6 

41479.2 

87.05 

4.4 

36107.6 

72%

188827 

60.9 

43848.0 

86.95 

4.3 

38125.8 

76%

200845 

67.4 

48556.8 

86.65 

4.1 

42074.5 

80%

211414 

73.8 

53100.0 

86.25 

4.0 

45798.8 

85%

222218 

80.9 

58248.0 

85.69 

3.8 

49912.7 

100%

234190 

89.6 

64533.6 

84.97 

3.6 

54834.2 

*The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, for reference only.
MSC 64x23-P-780V Load Performance Parameters of Upper Rotor of Coaxial
MSC 64x23-P-780V Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Efficiency(%)

Efficiency(g/W)

Power Output(W)

Temperature(℃)

780V

MSC 64x23-P

38%

63322

11.6

9024.6

81.50

7.0

7355.0

/

40%

70468 

13.4 

10467.6 

82.50 

6.7 

8635.8 

42%

77776 

15.4 

12019.8 

83.32 

6.5 

10014.9 

44%

85222 

17.5 

13681.2 

84.00 

6.2 

11492.2 

46%

92781 

19.8 

15436.2 

84.56 

6.0 

13052.9 

48%

100426 

22.2 

17292.6 

85.03 

5.8 

14703.9 

50%

108132 

24.7 

19227.0 

85.43 

5.6 

16425.6 

52%

115873 

27.2 

21231.6 

85.76 

5.5 

18208.2 

54%

123621 

29.9 

23306.4 

86.03 

5.3 

20050.5 

56%

131349 

32.6 

25451.4 

86.25 

5.2 

21951.8 

58%

139029 

35.4 

27643.2 

86.43 

5.0 

23892.0 

60%

146630 

38.3 

29889.6 

86.57 

4.9 

25875.4 

62%

154125 

41.3 

32175.0 

86.66 

4.8 

27882.9 

64%

161481 

44.2 

34499.4 

86.71 

4.7 

29914.4 

66%

168669 

47.3 

36855.0 

86.72 

4.6 

31960.7 

68%

175656 

50.3 

39241.8 

86.69 

4.5 

34018.7 

70%

182409 

53.4 

41636.4 

86.62 

4.4 

36065.4 

72%

188895 

56.5 

44046.6 

86.53 

4.3 

38113.5 

76%

200925 

62.6 

48804.6 

86.24 

4.1 

42089.1 

80%

211457 

68.4 

53344.2 

85.89 

4.0 

45817.3 

85%

222052 

74.8 

58328.4 

85.42 

3.8 

49824.1 

100%

232212 

81.5 

63546.6 

84.87 

3.7 

53932.0 

*The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, for reference only.
MSC 73x21-P-720V Load Performance Parameters of Upper Rotor of Coaxial
MSC 73x21-P-720V Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Efficiency(%)

Efficiency(g/W)

Power Output(W)

Temperature(℃)

720V

MSC 73x21-P

38%

68486

12.1

8733.6

84.02

7.8

7338.0

/

40%

75793 

14.0 

10080.0 

84.76 

7.5 

8543.8 

42%

83240 

16.0 

11520.0 

85.39 

7.2 

9836.9 

44%

90784 

18.1 

13046.4 

85.91 

7.0 

11208.2 

46%

98391 

20.4 

14652.0 

86.32 

6.7 

12647.6 

48%

106027 

22.7 

16329.6 

86.63 

6.5 

14146.3 

50%

113665 

25.1 

18064.8 

86.86 

6.3 

15691.1 

52%

121281 

27.6 

19864.8 

87.02 

6.1 

17286.3 

54%

128850 

30.2 

21715.2 

87.11 

5.9 

18916.1 

56%

136354 

32.8 

23616.0 

87.16 

5.8 

20583.7 

58%

143774 

35.5 

25552.8 

87.17 

5.6 

22274.4 

60%

151093 

38.2 

27532.8 

87.15 

5.5 

23994.8 

62%

158294 

41.0 

29534.4 

87.10 

5.4 

25724.5 

64%

165361 

43.8 

31564.8 

87.04 

5.2 

27474.0 

66%

172278 

46.7 

33609.6 

86.96 

5.1 

29226.9 

68%

179027 

49.5 

35661.6 

86.86 

5.0 

30975.7 

70%

185590 

52.4 

37713.6 

86.75 

4.9 

32716.5 

72%

191946 

55.2 

39758.4 

86.63 

4.8 

34442.7 

76%

203948 

60.8 

43776.0 

86.32 

4.7 

37787.4 

80%

214819 

66.1 

47584.8 

85.92 

4.5 

40884.9 

85%

226396 

72.0 

51854.4 

85.31 

4.4 

44237.0 

100%

239930 

79.5 

57225.6 

84.36 

4.2 

48275.5 

*The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, for reference only.
MSC 73x21-P-780V Load Performance Parameters of Upper Rotor of Coaxial
MSC 73x21-P-780V Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Efficiency(%)

Efficiency(g/W)

Power Output(W)

Temperature(℃)

780V

MSC 73x21-P

38%

68365

11.2

8751.6

83.56

7.8

7312.8

/

40%

75618 

13.0 

10101.0 

84.30 

7.5 

8515.1 

42%

83025 

14.8 

11536.2 

84.92 

7.2 

9796.5 

44%

90546 

16.8 

13072.8 

85.43 

6.9 

11168.1 

46%

98144 

18.8 

14679.6 

85.84 

6.7 

12601.0 

48%

105784 

21.0 

16364.4 

86.17 

6.5 

14101.2 

50%

113438 

23.2 

18103.8 

86.43 

6.3 

15647.1 

52%

121078 

25.5 

19913.4 

86.63 

6.1 

17251.0 

54%

128680 

27.9 

21762.0 

86.76 

5.9 

18880.7 

56%

136222 

30.3 

23665.2 

86.84 

5.8 

20550.9 

58%

143684 

32.8 

25599.6 

86.88 

5.6 

22240.9 

60%

151045 

35.4 

27573.0 

86.87 

5.5 

23952.7 

62%

158289 

37.9 

29577.6 

86.83 

5.4 

25682.2 

64%

165397 

40.5 

31605.6 

86.77 

5.2 

27424.2 

66%

172352 

43.2 

33657.0 

86.67 

5.1 

29170.5 

68%

179135 

45.8 

35716.2 

86.55 

5.0 

30912.4 

70%

185728 

48.4 

37775.4 

86.42 

4.9 

32645.5 

72%

192110 

51.1 

39826.8 

86.27 

4.8 

34358.6 

76%

204154 

56.2 

43859.4 

85.92 

4.7 

37684.0 

80%

215063 

61.1 

47689.2 

85.54 

4.5 

40793.3 

85%

226720 

66.6 

51955.8 

85.04 

4.4 

44183.2 

100%

240858 

73.5 

57306.6 

84.25 

4.2 

48280.8 

*The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, for reference only.
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FAQ

P115M
Hobbywing P115 Drone Propulsion System
P115M
The Industry's First 800V Coaxial Integrated Propulsion System
Specially designed for firefighting tethered drones and heavy-lift cargo eVTOLs.
Max. input voltag850V DC
Max. thrust240kg
Highly Integrated
Innovative Design
Hobbywing P115 Drone Motor With Propeller
At 800V and over 100kg-class thrust, the motor, ESC, and propeller are fully integrated in a groundbreaking design that
eliminates exposed cables. This streamlines the entire wiring layout, drastically reduces installation complexity and
maintenance costs, and eliminates failures from cable tension, abrasion, or short circuits at the source.
Significantly Enhancing Overall System Reliability.
Ultra Short Wiring
Shortened Three-Phase Cables minimizes transmission losses and EMI from long runs.
Delivering Higher System Efficiency, Superior Stability, and Cleaner power Performance.
All wiring placed inside durable carbon tubes to resist aging, moisture ingress, salt spray corrosion, and dust.
Ensuring extended, maintenance-free lifespan in demanding applications.
Internal Support Design For Tube Clamp Holders
The patented internal support structure effectively suppresses vibration and displacement of
arms under heavy-lift conditions, ensuring continuous, stable, and reliable propulsion output.
Compatible with arm thicknesses ranging from 2 mm to 5 mm, accommodating a wide variety
of materials and manufacturing processes for maximum integration flexibility.
  • Highly integrated design
  • Ultra-short wiring
  • All built-in connections
  • Innovative patented internal support design for tube clip holder
Highly Integrated
Innovative Design
Hobbywing P115 Drone Motor With Propeller
Highly integrated design
At 800V and over 100kg-class thrust, the motor, ESC, and propeller are fully integrated in a groundbreaking design that eliminates exposed cables. This streamlines the entire wiring layout, drastically reduces installation complexity and maintenance costs, and eliminates failures from cable tension, abrasion, or short circuits at the source. Significantly Enhancing Overall System Reliability.
Ultra Short Wiring
Ultra-short wiring
Shortened Three-Phase Cables minimizes transmission losses and EMI from long runs. Delivering Higher System Efficiency, Superior Stability, and Cleaner power Performance.
All Built In Connections
All built-in connections
All wiring placed inside durable carbon tubes to resist aging, moisture ingress, salt spray corrosion, and dust. Ensuring extended, maintenance-free lifespan in demanding applications.
Internal Support Design For Tube Clamp Holders
Innovative patented internal support design for tube clip holder
The patented internal support structure effectively suppresses vibration and displacement of arms under heavy-lift conditions, ensuring continuous, stable, and reliable propulsion output. Compatible with arm thicknesses ranging from 2 mm to 5 mm, accommodating a wide variety of materials and manufacturing processes for maximum integration flexibility.
800V High-Voltage SiC Platform
Efficient Energy-Saving
Supports 810v Dc Input
Supports 850V DC input, reaching the top
industrial standard.
At the same power level, transmission current is significantly reduced, minimizing energy losses, allowing thinner and lighter cables, and substantially increasing overall power density.
Automotive Sic Mosfets
Equipped with cutting-edge third-generation automotive-grade SiC MOSFETs, the system achieves ultra-low switching losses and a substantial boost in overall efficiency. Ideal for demanding, mission-critical applications such as firefighting, cargo transport, and heavy-lift industrial operations.
Broad Compatibility &
Flexible Adaptation

Compatible with D60 and D80 arm mount methods,

the product supports both flat and coaxial layouts,

and offers 64-inch and 73-inch quick-release carbon fiber propellers,

meeting the overall size requirements.

P115 Drone Motor With Carbon Fiber Propeller
Robust Protection,
Ready for Harsh Environments

The motor features high-temperature resistant enameled wires rated up to 200°C, an IPX5

protection rating, and insulation capable of withstanding up to 2,700V. The system’s internal potting

process provides robust protection against high temperatures, humidity, and firefighting powders.

Rated
up to
200℃

Protection rating
IPX5

Withstanding up to
2700V
High Temperature Resistant Enameled WireHigh-temperature
resistant enameled wires
Ipx5 Waterproof Drone Motor
Multiple Redundancy
Designs for a Safer Flight
Control redundancy

The product boasts dual-mode operation with sensorless FOC as the primary

control and sensor FOC as backup for enhanced safety. Two sets of signal channels

can be converted in real time to enhance the reliability of the propulsion system./p>

Real Time Signal Channel Conversion

Communication redundancy

The dual heterogeneous communication links via CAN bus and RS485 are supported.

Speed information is obtained in real time through dual channels to meet airworthiness

certification requirements and flexibly respond to future regulatory requirements.

Motor Supporting Can Bus And Rs485 Communication
Throttle redundancy

Three throttle combination methods are supported

PWM+CAN digital throttle
is the default configuration
PWM+RS485
is optional
CAN+RS485
is optional

Adapts seamlessly to the communication needs of various flight controllers, enabling real-time

upload of critical flight data and continuous monitoring of key parameters.

(RPM, Throttle Position, Current, Voltage, and Temperature)

Hobbywing P65m Powerful Drone Motor
Two types of power distribution schemes

In addition to conventional high‑voltage input, it also supports an

independent high and low voltage power distribution method (with low

voltage at 24V). Both power distribution schemes are fully compatible.

Independent High And Low Voltage Distribution Method
Reliable Design,
Automotive-Grade Materialsn

Automotive-Grade System Design

Modular Design
The software
adopts a rigorous modular design.
High Voltage Drone Propulsion System
The hardware 
system implements a fully isolated architecture, separating high-voltage power circuits, low-voltage signal circuits, and protective earthing (PE). This ensures reliable data transmission, stable equipment operation, and significantly enhanced safety for both personnel and connected systems.
  • Structural
    design
  • High-
    specification
    materials
  • Tilt design
    of the tube
    clip holder
Coaxial Drone Motor
Structural design
The dual-rotor coaxial structure significantly shortens arm length and
enhances effective payload space. In addition, the product features a
sleek and streamlined design with no exposed cables.
Vtol Drone Electric Motor And Esc
High-specification materials
The ESCs feature automotive-grade components, motors are crafted from
high-temperature-resistant materials, propellers are made of carbon fiber materials
with higher reliability, and connectors adopt automotive-grade materials, which are
foolproof, anti-false connection and vibration-resistant, providing reliable system
connection and extended service life.
3° Tube Clamp Holder Tilt Design
Tilt design of the tube clip holder
The 3° tube clip holder tilt design improves coaxial flight control efficiency,
hovering stability, and maneuverability, easily adaptable to various flight controllers.
Multiple Protection Functions
Throttle loss
warning
Reverse polarity
protection
Undervoltage
warning
Overvoltage
warning
Overcurrent
protection
Over-temperature
warning
Motor stall
protection
Motor overspeed
protection
Fail to reset throttle
to zero protection
Fault Storage & Black Box
Black Box Data Recording
The fault storage function
can record fault codes during
operation, making it easier to
accurately trace the cause.
Real-time recording of UAV operation
data within 2-48 hours facilitates
subsequent data analysis.
Fault Storage Function
The black box
captures real-time operational
data with milliseconds, allowing
for traceability and analysis.
Fast Parameter Adjustment
and Firmware OTA Upgrade

With HOBBYWING’s proprietary host computer software, users can adjust drive

parameters, motor rotation direction, and light color (default green) effortlessly based on

application requirements to optimize flight performance and upgrade the latest firmware.

Parameter Adjustment And Firmware Ota Upgrade
P115M & MSC 64×23-P Overload Curve
Test Voltage: 720V

  • *he above data provides the maximum permissible temperature values for each overload point, measured under optimal conditions: effective heat dissipation, an ambient temperature of 25°C, sea-level altitude, and consistent rotational speed.
  • The horizontal axis (time) represents the maximum safe operating duration for each overload point under the stated conditions. Exceeding this duration during actual flight may cause irreversible damage to the propulsion system due to overheating.
  • Please note: To prioritize flight safety, the propulsion system will not automatically shut down. Therefore, strict monitoring is required to avoid overloading beyond the specified time limits.
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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P115M CAD
MSC 64×23-P CAD
MSC 73×21-P CAD
Product Name P115M
  • MSC 64x23-P
  • MSC 73x21-P (Coming soon)
Integrated thrust system specification
  • Model
  • Max Thrust
  • Rated thrust
  • System efficiency
  • Input voltage
  • Rated voltage
  • Tube outer diameter
  • Weight(with cable and Props)
  • Cable specification
  • Operating temperature
  • Ingress protection
  • Rated power input(single motor)
  • Rated power output(single motor)
  • Signal cable define
  • P115M
  • 234 kg
  • 115 kg
  • 5.5 g/W
  • 500~850V
  • 720 V
  • Φ80mm(Wall thickness varies by material, ends require specific holes. See specs.)
  • 19.7 kg ± 50 g
  • Power cable:12AWG*2000 mm Signal cable:2200 mm
  • -35~55 ℃
  • IP35
  • 10608 W
  • 9121 W
  • Blue-CAN-GND、Red-CANH,Brown-CANL、Black-Shielded、Green-PWM、,Gray-PWM-GND、Orange-DC24V+、Yellow-DC24V-
  • P115M
  • 240 kg
  • 115 kg
  • 6.2 g/W
  • 500~850V
  • 720 V
  • Φ80mm(Wall thickness varies by material, ends require specific holes. See specs.)
  • 20.1 kg ±150 g
  • Power cable:12AWG*2000 mm Signal cable:2200 mm
  • -35~55 ℃
  • IP35
  • 9650 W
  • 8400 W
  • Blue-CAN-GND、Red-CANH,Brown-CANL、Black-Shielded、Green-PWM、,Gray-PWM-GND、Orange-DC24V+、Yellow-DC24V-
ESC specification
  • Rated voltage
  • Communication protocol
  • ESC size
  • Weight(with cable)
  • Peak current (10 seconds)
  • Continuous current
  • Ingress Protection
  • Double throttle signal
  • Operating pulse width(Not supported)
  • Black box
  • 720 V
  • CAN(customizable RS485)
  • 211 mm*104 mm*67 mm(Without plug)
  • 1880±50 g
  • 45 A
  • 15 A
  • IP67
  • CAN+RS485 / CAN+PWM / RS485+PWM
  • 1100~1940 μs
  • 2~48h log
  • 720 V
  • CAN(customizable RS485)
  • 211 mm*104 mm*67 mm(Without plug)
  • 1880±50 g
  • 45 A
  • 15 A
  • IP67
  • CAN+RS485 / CAN+PWM / RS485+PWM
  • 1100~1940 μs
  • 2~48h log
Motor specification
  • Stator size
  • KV
  • Motor diameter
  • Slot& Pole
  • Ingress Protection
  • Weight(with cable)
  • 156*50 mm
  • 5.5 KV
  • Φ167.1±0.1 mm
  • 36N42P
  • IPX5
  • 5172 g
  • 156*50 mm
  • 5KV
  • Φ167.1±0.1 mm
  • 36N42P
  • IPX5
  • 5182 g
Propeller specification
  • Model
  • Weight
  • Material of Props
  • Mounting dimensions
  • MSC 64x23-P
  • 1035 g
  • Carbon unfolding Props
  • D60-6*M6, centre hole D20
  • MSC 73x21-P
  • 1254 g
  • Carbon unfolding Props
  • D60-6*M6, centre hole D20
MSC 64x23-P-720V Load Performance Parameters of Upper Rotor of Coaxial
MSC 64x23-P-720V Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Efficiency(%)

Efficiency(g/W)

Power Output(W)

Temperature(℃)

720V

MSC 64x23-P

38%

63370

12.5

9007.2

82.10

7.0

7394.9

/

40%

70510 

14.5 

10440.0 

83.09 

6.8 

8674.6 

42%

77805 

16.6 

11980.8 

83.92 

6.5 

10054.3 

44%

85235 

18.9 

13629.6 

84.60 

6.3 

11530.6 

46%

92777 

21.4 

15372.0 

85.17 

6.0 

13092.3 

48%

100409 

23.9 

17215.2 

85.62 

5.8 

14739.7 

50%

108106 

26.6 

19144.8 

86.00 

5.6 

16464.5 

52%

115840 

29.4 

21153.6 

86.30 

5.5 

18255.6 

54%

123586 

32.3 

23234.4 

86.54 

5.3 

20107.0 

56%

131313 

35.3 

25380.0 

86.74 

5.2 

22014.6 

58%

138994 

38.3 

27576.0 

86.89 

5.0 

23960.8 

60%

146597 

41.4 

29815.2 

87.01 

4.9 

25942.2 

62%

154091 

44.6 

32097.6 

87.08 

4.8 

27950.6 

64%

161446 

47.8 

34416.0 

87.13 

4.7 

29986.7 

66%

168629 

51.0 

36748.8 

87.14 

4.6 

32022.9 

68%

175608 

54.3 

39110.4 

87.11 

4.5 

34069.1 

70%

182351 

57.6 

41479.2 

87.05 

4.4 

36107.6 

72%

188827 

60.9 

43848.0 

86.95 

4.3 

38125.8 

76%

200845 

67.4 

48556.8 

86.65 

4.1 

42074.5 

80%

211414 

73.8 

53100.0 

86.25 

4.0 

45798.8 

85%

222218 

80.9 

58248.0 

85.69 

3.8 

49912.7 

100%

234190 

89.6 

64533.6 

84.97 

3.6 

54834.2 

*The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, for reference only.
MSC 64x23-P-780V Load Performance Parameters of Upper Rotor of Coaxial
MSC 64x23-P-780V Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Efficiency(%)

Efficiency(g/W)

Power Output(W)

Temperature(℃)

780V

MSC 64x23-P

38%

63322

11.6

9024.6

81.50

7.0

7355.0

/

40%

70468 

13.4 

10467.6 

82.50 

6.7 

8635.8 

42%

77776 

15.4 

12019.8 

83.32 

6.5 

10014.9 

44%

85222 

17.5 

13681.2 

84.00 

6.2 

11492.2 

46%

92781 

19.8 

15436.2 

84.56 

6.0 

13052.9 

48%

100426 

22.2 

17292.6 

85.03 

5.8 

14703.9 

50%

108132 

24.7 

19227.0 

85.43 

5.6 

16425.6 

52%

115873 

27.2 

21231.6 

85.76 

5.5 

18208.2 

54%

123621 

29.9 

23306.4 

86.03 

5.3 

20050.5 

56%

131349 

32.6 

25451.4 

86.25 

5.2 

21951.8 

58%

139029 

35.4 

27643.2 

86.43 

5.0 

23892.0 

60%

146630 

38.3 

29889.6 

86.57 

4.9 

25875.4 

62%

154125 

41.3 

32175.0 

86.66 

4.8 

27882.9 

64%

161481 

44.2 

34499.4 

86.71 

4.7 

29914.4 

66%

168669 

47.3 

36855.0 

86.72 

4.6 

31960.7 

68%

175656 

50.3 

39241.8 

86.69 

4.5 

34018.7 

70%

182409 

53.4 

41636.4 

86.62 

4.4 

36065.4 

72%

188895 

56.5 

44046.6 

86.53 

4.3 

38113.5 

76%

200925 

62.6 

48804.6 

86.24 

4.1 

42089.1 

80%

211457 

68.4 

53344.2 

85.89 

4.0 

45817.3 

85%

222052 

74.8 

58328.4 

85.42 

3.8 

49824.1 

100%

232212 

81.5 

63546.6 

84.87 

3.7 

53932.0 

*The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, for reference only.
MSC 73x21-P-720V Load Performance Parameters of Upper Rotor of Coaxial
MSC 73x21-P-720V Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Efficiency(%)

Efficiency(g/W)

Power Output(W)

Temperature(℃)

720V

MSC 73x21-P

38%

68486

12.1

8733.6

84.02

7.8

7338.0

/

40%

75793 

14.0 

10080.0 

84.76 

7.5 

8543.8 

42%

83240 

16.0 

11520.0 

85.39 

7.2 

9836.9 

44%

90784 

18.1 

13046.4 

85.91 

7.0 

11208.2 

46%

98391 

20.4 

14652.0 

86.32 

6.7 

12647.6 

48%

106027 

22.7 

16329.6 

86.63 

6.5 

14146.3 

50%

113665 

25.1 

18064.8 

86.86 

6.3 

15691.1 

52%

121281 

27.6 

19864.8 

87.02 

6.1 

17286.3 

54%

128850 

30.2 

21715.2 

87.11 

5.9 

18916.1 

56%

136354 

32.8 

23616.0 

87.16 

5.8 

20583.7 

58%

143774 

35.5 

25552.8 

87.17 

5.6 

22274.4 

60%

151093 

38.2 

27532.8 

87.15 

5.5 

23994.8 

62%

158294 

41.0 

29534.4 

87.10 

5.4 

25724.5 

64%

165361 

43.8 

31564.8 

87.04 

5.2 

27474.0 

66%

172278 

46.7 

33609.6 

86.96 

5.1 

29226.9 

68%

179027 

49.5 

35661.6 

86.86 

5.0 

30975.7 

70%

185590 

52.4 

37713.6 

86.75 

4.9 

32716.5 

72%

191946 

55.2 

39758.4 

86.63 

4.8 

34442.7 

76%

203948 

60.8 

43776.0 

86.32 

4.7 

37787.4 

80%

214819 

66.1 

47584.8 

85.92 

4.5 

40884.9 

85%

226396 

72.0 

51854.4 

85.31 

4.4 

44237.0 

100%

239930 

79.5 

57225.6 

84.36 

4.2 

48275.5 

*The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, for reference only.
MSC 73x21-P-780V Load Performance Parameters of Upper Rotor of Coaxial
MSC 73x21-P-780V Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Efficiency(%)

Efficiency(g/W)

Power Output(W)

Temperature(℃)

780V

MSC 73x21-P

38%

68365

11.2

8751.6

83.56

7.8

7312.8

/

40%

75618 

13.0 

10101.0 

84.30 

7.5 

8515.1 

42%

83025 

14.8 

11536.2 

84.92 

7.2 

9796.5 

44%

90546 

16.8 

13072.8 

85.43 

6.9 

11168.1 

46%

98144 

18.8 

14679.6 

85.84 

6.7 

12601.0 

48%

105784 

21.0 

16364.4 

86.17 

6.5 

14101.2 

50%

113438 

23.2 

18103.8 

86.43 

6.3 

15647.1 

52%

121078 

25.5 

19913.4 

86.63 

6.1 

17251.0 

54%

128680 

27.9 

21762.0 

86.76 

5.9 

18880.7 

56%

136222 

30.3 

23665.2 

86.84 

5.8 

20550.9 

58%

143684 

32.8 

25599.6 

86.88 

5.6 

22240.9 

60%

151045 

35.4 

27573.0 

86.87 

5.5 

23952.7 

62%

158289 

37.9 

29577.6 

86.83 

5.4 

25682.2 

64%

165397 

40.5 

31605.6 

86.77 

5.2 

27424.2 

66%

172352 

43.2 

33657.0 

86.67 

5.1 

29170.5 

68%

179135 

45.8 

35716.2 

86.55 

5.0 

30912.4 

70%

185728 

48.4 

37775.4 

86.42 

4.9 

32645.5 

72%

192110 

51.1 

39826.8 

86.27 

4.8 

34358.6 

76%

204154 

56.2 

43859.4 

85.92 

4.7 

37684.0 

80%

215063 

61.1 

47689.2 

85.54 

4.5 

40793.3 

85%

226720 

66.6 

51955.8 

85.04 

4.4 

44183.2 

100%

240858 

73.5 

57306.6 

84.25 

4.2 

48280.8 

*The above data is measured by HobbyWing laboratory at room temperature 25℃, sea level, change the throttle input adjustment, for reference only.
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