Buy |
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 |
VSC 60x20 |
33% |
24355 |
7.7 |
2590.5 |
1386 |
9.4 |
14.31 |
2076.8 |
87℃ |
|
35% |
27794 |
9.3 |
3105.6 |
1481 |
8.9 |
16.33 |
2532.6 |
|||
|
37% |
31375 |
11.0 |
3675.3 |
1574 |
8.5 |
18.45 |
3040.5 |
|||
|
39% |
35078 |
12.8 |
4298.9 |
1663 |
8.2 |
20.65 |
3595.3 |
|||
|
42% |
40817 |
15.9 |
5331.5 |
1792 |
7.7 |
24.07 |
4517.4 |
|||
|
45% |
46718 |
19.3 |
6474.9 |
1914 |
7.2 |
27.62 |
5536.0 |
|||
|
48% |
52718 |
23.0 |
7720.3 |
2030 |
6.8 |
31.25 |
6643.3 |
|||
|
51% |
58756 |
27.0 |
9057.8 |
2140 |
6.5 |
34.93 |
7827.4 |
|||
|
54% |
64775 |
31.3 |
10475.5 |
2245 |
6.2 |
38.62 |
9078.8 |
|||
|
57% |
70721 |
35.7 |
11960.0 |
2344 |
5.9 |
42.29 |
10379.3 |
|||
|
60% |
76540 |
40.3 |
13496.2 |
2437 |
5.7 |
45.90 |
11712.7 |
|||
|
63% |
82184 |
45.0 |
15066.5 |
2524 |
5.5 |
49.42 |
13061.5 |
|||
|
66% |
87605 |
49.7 |
16651.2 |
2604 |
5.3 |
52.82 |
14402.1 |
|||
|
69% |
92757 |
54.4 |
18228.5 |
2677 |
5.1 |
56.06 |
15714.7 |
|||
|
72% |
97598 |
59.0 |
19774.6 |
2744 |
4.9 |
59.11 |
16985.4 |
|||
|
75% |
102087 |
63.5 |
21264.1 |
2804 |
4.8 |
61.95 |
18189.1 |
|||
|
78% |
106183 |
67.7 |
22670.8 |
2858 |
4.7 |
64.54 |
19313.5 |
|||
|
81% |
109849 |
71.5 |
23968.0 |
2905 |
4.6 |
66.85 |
20334.3 |
|||
|
84% |
113049 |
75.0 |
25129.8 |
2946 |
4.5 |
68.86 |
21242.4 |
|||
|
87% |
115749 |
78.0 |
26130.9 |
2981 |
4.4 |
70.55 |
22023.2 |
|||
|
100% |
116531 |
78.9 |
26424.7 |
2991 |
4.4 |
71.04 |
22250.4 |
-
Drone Propulsion Systems
-
- INTEGRATED PROPULSION SYSTEM Innovation and Performance for a simplified assembly.
- X Series
- H Series
- P Series
-
-
-
- PROPELLER Superior efficiency, exceptional stability.
- Carbon Plastic Propeller
- Carbon Fiber Propeller
-
- CENTRIFUGAL NOZZLE Efficient atomizing, precise spraying.
- 9L
-
- WATER PUMP Minimal maintenance, long service life.
- 5L
- 8L
- 30L
-
- PROPULSION SYSTEM Innovation and Performance for a simplified assembly.
- P Series
-
-
-
- PROPELLER Powerful burst, high intensity.
- Carbon Fiber Propeller
-
-
RC Power Systems
RC Cars Power SystemRC Boat Power System
-
e-Vehicle Power Systems
Electric MotorcycleElectric SkateboardElectric Scooter
- Service and Support
- Software
- Adopts rigorous modularized design and various
redundancy strategies.
- Hardware
- The Protective Earth (PE) is completely isolated from the
high-voltage power circuits and low-voltage signal circuits,
ensuring superior system reliability.
of the Position Sensor
- The flexible setting of the propeller stopping position
- Reduces the resistance of the UAV during cruise
- flight and extends the flight endurance.
of the Position Sensor
- The flexible setting of the propeller stopping position
- Reduces the resistance of the UAV during cruise
- flight and extends the flight endurance.
- The propeller is aerodynamically optimized
- with a large aspect ratio, a small windward side,
- and a propeller tip with a low wind resistance,
- striking an optimal balance between efficiency and thrust capacity.
- This design is tailored for the specific application requirements of VTOLs.
- Obtain RPM information in real time through dual channels
- to meet airworthiness certification requirements and
- easily respond to future regulatory requirements.
High Reliability Technology Process
- ESC
- Motor
- Propeller
- Automotive-Grade Connectors
- The ESC uses automotive-grade
components with higher
temperature resistance.
- The motor is made of high temperature resistant material,
combined with the dual design of knurl shaft
and screws to avoid loosening.
- The propeller adopts carbon fiber molding process.
- Both high-voltage and low-voltage signal connectors are
constructed with automotive-grade materials,
featuring fool-proof design,
prevention of poor contact, and vibration resistance.
This ensures reliable system connectivity and extended service life.
High Reliability Technology Process
- ESC
- The ESC uses automotive-grade components with higher
temperature resistance.
- Motor
- The motor is made of high temperature resistant material,
combined with the dual design of knurl shaft
and screws to avoid loosening.
- Propeller
- The propeller adopts carbon fiber molding process.
- Automotive-Grade Connectors
- Both high-voltage and low-voltage signal connectors are
constructed with automotive-grade materials,
featuring fool-proof design,
prevention of poor contact, and vibration resistance.
This ensures reliable system connectivity and extended service life.
and Triple Throttle Control Modes
ensuring the safety of personnel during every debugging and testing session.
Triple throttle control modes are as follows:
- CAN+RS485
- is the default configuration
- CAN+PWM
- is optional
- RS485+PWM
- is optional
enabling real-time data transmission and
continuous monitoring of critical flight parameters
(including RPM, throttle position, current, voltage and temperature).
This integrated solution enables rapid data analysis,
prompt response to issues, and significantly enhancing flight safety.
for Added Security
A physical RPM sensor is used to directly obtain the RPM signal for motor control
Without a physical RPM sensor, the RPM signal is obtained through software algorithms
verified by over 1000 hours of continuous aging testing,
ensures maintenance-free operation throughout its entire lifecycle
developed and designed by HOBBYWING,
ensuring meticulous attention to every detail
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.
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.
Compatibility
ArduPilot open-source ecosystem, VK, Byaero and Jiyi,
supports CAN communication, and builds an intelligent flight ecosystem.
Feedback of Coil Temperature
- *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.
- *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.
| Product Name |
|
||||||||||||||||||||||||||||
| Specifications |
|
||||||||||||||||||||||||||||
| ESC specification |
|
||||||||||||||||||||||||||||
| Motor specification |
|
||||||||||||||||||||||||||||
| Propeller |
|
||||||||||||||||||||||||||||
|
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 |
VSC 60x20 |
33% |
24252 |
6.5 |
2613.6 |
1387 |
9.3 |
14.29 |
2074.9 |
89℃ |
|
35% |
27683 |
7.8 |
3128.6 |
1480 |
8.8 |
16.33 |
2530.4 |
|||
|
37% |
31272 |
9.3 |
3705.1 |
1572 |
8.4 |
18.46 |
3038.0 |
|||
|
39% |
34997 |
10.8 |
4339.1 |
1662 |
8.1 |
20.66 |
3595.6 |
|||
|
42% |
40798 |
13.5 |
5388.5 |
1793 |
7.6 |
24.09 |
4523.1 |
|||
|
45% |
46790 |
16.4 |
6544.6 |
1916 |
7.1 |
27.64 |
5546.0 |
|||
|
48% |
52899 |
19.5 |
7796.8 |
2033 |
6.8 |
31.28 |
6659.6 |
|||
|
51% |
59049 |
22.8 |
9137.3 |
2142 |
6.5 |
34.98 |
7845.3 |
|||
|
54% |
65167 |
26.4 |
10559.2 |
2245 |
6.2 |
38.69 |
9095.0 |
|||
|
57% |
71180 |
30.1 |
12053.0 |
2342 |
5.9 |
42.38 |
10392.2 |
|||
|
60% |
77023 |
34.0 |
13604.3 |
2434 |
5.7 |
46.00 |
11722.9 |
|||
|
63% |
82633 |
38.0 |
15191.9 |
2522 |
5.4 |
49.50 |
13072.8 |
|||
|
66% |
87959 |
42.0 |
16788.6 |
2604 |
5.2 |
52.85 |
14411.8 |
|||
|
69% |
92958 |
45.9 |
18362.6 |
2679 |
5.1 |
56.01 |
15712.8 |
|||
|
72% |
97596 |
49.7 |
19881.7 |
2747 |
4.9 |
58.95 |
16955.4 |
|||
|
75% |
101855 |
53.3 |
21317.1 |
2807 |
4.8 |
61.63 |
18115.8 |
|||
|
78% |
105731 |
56.6 |
22646.8 |
2858 |
4.7 |
64.07 |
19173.3 |
|||
|
81% |
109236 |
59.6 |
23858.5 |
2901 |
4.6 |
66.25 |
20125.1 |
|||
|
84% |
112399 |
62.4 |
24951.0 |
2935 |
4.5 |
68.20 |
20961.0 |
|||
|
87% |
115272 |
64.8 |
25934.1 |
2962 |
4.4 |
69.96 |
21697.3 |
|||
|
100% |
116176 |
65.6 |
26240.6 |
2970 |
4.4 |
70.50 |
21926.1 |
|
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 |
USC 54x23 |
33% |
22163 |
7.6 |
2532.7 |
1487 |
8.8 |
12.90 |
2009.3 |
90℃ |
|
35% |
25389 |
9.1 |
3046.0 |
1589 |
8.3 |
14.79 |
2461.3 |
|||
|
37% |
28798 |
10.8 |
3625.0 |
1691 |
7.9 |
16.80 |
2974.5 |
|||
|
39% |
32358 |
12.7 |
4266.6 |
1790 |
7.6 |
18.90 |
3543.3 |
|||
|
42% |
37913 |
15.9 |
5337.2 |
1934 |
7.1 |
22.21 |
4498.1 |
|||
|
45% |
43650 |
19.5 |
6525.9 |
2070 |
6.7 |
25.65 |
5560.2 |
|||
|
48% |
49496 |
23.3 |
7819.8 |
2198 |
6.3 |
29.18 |
6716.2 |
|||
|
51% |
55388 |
27.5 |
9208.1 |
2318 |
6.0 |
32.76 |
7951.5 |
|||
|
54% |
61275 |
31.9 |
10680.7 |
2431 |
5.7 |
36.36 |
9254.5 |
|||
|
56% |
65173 |
34.9 |
11704.4 |
2503 |
5.6 |
38.75 |
10155.6 |
|||
|
60% |
72850 |
41.3 |
13838.0 |
2638 |
5.3 |
43.48 |
12011.8 |
|||
|
63% |
78456 |
46.3 |
15497.4 |
2732 |
5.1 |
46.97 |
13436.0 |
|||
|
66% |
83886 |
51.3 |
17187.6 |
2820 |
4.9 |
50.36 |
14870.5 |
|||
|
69% |
89094 |
56.4 |
18884.7 |
2901 |
4.7 |
53.63 |
16292.4 |
|||
|
72% |
94030 |
61.4 |
20559.0 |
2975 |
4.6 |
56.76 |
17681.0 |
|||
|
75% |
98634 |
66.2 |
22174.3 |
3041 |
4.4 |
59.69 |
19007.4 |
|||
|
78% |
102836 |
70.7 |
23688.3 |
3098 |
4.3 |
62.39 |
20238.0 |
|||
|
81% |
106549 |
74.8 |
25053.6 |
3145 |
4.3 |
64.79 |
21335.0 |
|||
|
84% |
109674 |
78.3 |
26218.3 |
3183 |
4.2 |
66.82 |
22269.9 |
|||
|
87% |
112092 |
81.0 |
27126.4 |
3211 |
4.1 |
68.40 |
22997.1 |
|||
|
100% |
112716 |
81.7 |
27361.9 |
3218 |
4.1 |
68.81 |
23185.3 |
|
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 |
USC 54x23 |
33% |
22233 |
6.4 |
2577.3 |
1487 |
8.6 |
12.93 |
2013.1 |
92℃ |
|
35% |
25510 |
7.7 |
3096.2 |
1590 |
8.2 |
14.84 |
2470.4 |
|||
|
37% |
28943 |
9.2 |
3684.7 |
1691 |
7.9 |
16.86 |
2986.1 |
|||
|
39% |
32504 |
10.8 |
4336.8 |
1790 |
7.5 |
18.99 |
3558.5 |
|||
|
42% |
38033 |
13.6 |
5420.3 |
1933 |
7.0 |
22.30 |
4513.3 |
|||
|
45% |
43720 |
16.5 |
6613.4 |
2069 |
6.6 |
25.72 |
5571.5 |
|||
|
48% |
49499 |
19.8 |
7901.9 |
2197 |
6.3 |
29.20 |
6716.5 |
|||
|
51% |
55312 |
23.2 |
9276.3 |
2318 |
6.0 |
32.70 |
7937.8 |
|||
|
54% |
61107 |
26.8 |
10731.0 |
2431 |
5.7 |
36.22 |
9219.9 |
|||
|
56% |
64937 |
29.4 |
11743.1 |
2503 |
5.5 |
38.56 |
10106.8 |
|||
|
60% |
72465 |
34.6 |
13859.7 |
2638 |
5.2 |
43.22 |
11938.9 |
|||
|
63% |
77950 |
38.8 |
15515.2 |
2732 |
5.0 |
46.67 |
13351.7 |
|||
|
66% |
83258 |
43.0 |
17209.8 |
2820 |
4.8 |
50.06 |
14782.0 |
|||
|
69% |
88357 |
47.3 |
18919.3 |
2901 |
4.7 |
53.35 |
16205.9 |
|||
|
72% |
93213 |
51.5 |
20613.1 |
2974 |
4.5 |
56.50 |
17594.8 |
|||
|
75% |
97792 |
55.6 |
22256.4 |
3040 |
4.4 |
59.47 |
18929.3 |
|||
|
78% |
102057 |
59.5 |
23812.3 |
3097 |
4.3 |
62.20 |
20170.6 |
|||
|
81% |
105970 |
63.1 |
25244.6 |
3145 |
4.2 |
64.65 |
21292.0 |
|||
|
84% |
109488 |
66.3 |
26520.7 |
3185 |
4.1 |
66.80 |
22276.8 |
|||
|
87% |
112562 |
69.0 |
27614.1 |
3216 |
4.1 |
68.59 |
23099.2 |
|||
|
100% |
113479 |
69.8 |
27934.3 |
3224 |
4.1 |
69.11 |
23332.2 |
Support
Manuals & Documents
Disclaimer
The purpose of this website is only to introduce you to the basic situation of HOBBYWING company and product information. Unless otherwise stated, all information provided on this website should not be regarded as an offer or acceptance, and this website will not assume any binding obligations to you as a result of the provision of information. For all your requests, HOBBYWING reserves the full right to decide whether to commit or not.
This Website and its contents are provided for your convenience on an "as is" basis and your use of this Website is at your sole risk. HOBBYWING does not guarantee that this website will be uninterrupted or error-free, and reserves the right to amend this website or withdraw access to this Website at any time. We make no warranties, express or implied, as to the content, existence, accuracy or reliability of this Website, including, but not limited to, warranties of title, non-infringement or implied warranties of merchantability or fitness for a particular purpose or use.
HOBBYWING shall not be liable for any direct, indirect, incidental, special or consequential damages, loss of profits or business interruption caused by the use or inability to use the services provided by the Website, even if HOBBYWING has been advised of the possibility of similar losses. The exclusions and limitations of the warranty liability of HOBBYWING shall be effective to the extent permitted by applicable law.
HOBBYWING shall not be liable for any damage or loss to your computer system or any other software, hardware, IT system or property caused by viruses or other destructive programs caused by accessing, viewing and using this website or downloading any content from this Website (including but not limited to 2D model files, 3D model files).
HOBBYWING shall not be liable for any direct or indirect damage or loss caused by any third party using illegal means to access the website to obtain the relevant passwords, information and content.
If you or your company is located in the United States or Canada, you need to fill out this disclaimer confirmation letter online and submit it successfully before you can download the relevant materials you are interested in. The link address you fill in online is https://www.hobbywingdirect.com/pages/digital-file-release-form
If you do not agree with this disclaimer, please do not continue to this page. If you continue to access, browse and use this interface, you have read, understood and agreed to be bound by this statement and comply with all applicable laws and regulations.
HOBBYWING reserves the right to correct, modify and update this statement at any time.
- Software
- Adopts rigorous modularized design and various
redundancy strategies.
- Hardware
- The Protective Earth (PE) is completely isolated from the
high-voltage power circuits and low-voltage signal circuits,
ensuring superior system reliability.
of the Position Sensor
- The flexible setting of the propeller stopping position
- Reduces the resistance of the UAV during cruise
- flight and extends the flight endurance.
of the Position Sensor
- The flexible setting of the propeller stopping position
- Reduces the resistance of the UAV during cruise
- flight and extends the flight endurance.
- The propeller is aerodynamically optimized
- with a large aspect ratio, a small windward side,
- and a propeller tip with a low wind resistance,
- striking an optimal balance between efficiency and thrust capacity.
- This design is tailored for the specific application requirements of VTOLs.
- Obtain RPM information in real time through dual channels
- to meet airworthiness certification requirements and
- easily respond to future regulatory requirements.
High Reliability Technology Process
- ESC
- Motor
- Propeller
- Automotive-Grade Connectors
- The ESC uses automotive-grade
components with higher
temperature resistance.
- The motor is made of high temperature resistant material,
combined with the dual design of knurl shaft
and screws to avoid loosening.
- The propeller adopts carbon fiber molding process.
- Both high-voltage and low-voltage signal connectors are
constructed with automotive-grade materials,
featuring fool-proof design,
prevention of poor contact, and vibration resistance.
This ensures reliable system connectivity and extended service life.
High Reliability Technology Process
- ESC
- The ESC uses automotive-grade components with higher
temperature resistance.
- Motor
- The motor is made of high temperature resistant material,
combined with the dual design of knurl shaft
and screws to avoid loosening.
- Propeller
- The propeller adopts carbon fiber molding process.
- Automotive-Grade Connectors
- Both high-voltage and low-voltage signal connectors are
constructed with automotive-grade materials,
featuring fool-proof design,
prevention of poor contact, and vibration resistance.
This ensures reliable system connectivity and extended service life.
and Triple Throttle Control Modes
ensuring the safety of personnel during every debugging and testing session.
Triple throttle control modes are as follows:
- CAN+RS485
- is the default configuration
- CAN+PWM
- is optional
- RS485+PWM
- is optional
enabling real-time data transmission and
continuous monitoring of critical flight parameters
(including RPM, throttle position, current, voltage and temperature).
This integrated solution enables rapid data analysis,
prompt response to issues, and significantly enhancing flight safety.
for Added Security
A physical RPM sensor is used to directly obtain the RPM signal for motor control
Without a physical RPM sensor, the RPM signal is obtained through software algorithms
verified by over 1000 hours of continuous aging testing,
ensures maintenance-free operation throughout its entire lifecycle
developed and designed by HOBBYWING,
ensuring meticulous attention to every detail
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.
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.
Compatibility
ArduPilot open-source ecosystem, VK, Byaero and Jiyi,
supports CAN communication, and builds an intelligent flight ecosystem.
Feedback of Coil Temperature
- *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.
- *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.
| Product Name |
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| Specifications |
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| ESC specification |
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| Motor specification |
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| Propeller |
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|
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 |
VSC 60x20 |
33% |
24355 |
7.7 |
2590.5 |
1386 |
9.4 |
14.31 |
2076.8 |
87℃ |
|
35% |
27794 |
9.3 |
3105.6 |
1481 |
8.9 |
16.33 |
2532.6 |
|||
|
37% |
31375 |
11.0 |
3675.3 |
1574 |
8.5 |
18.45 |
3040.5 |
|||
|
39% |
35078 |
12.8 |
4298.9 |
1663 |
8.2 |
20.65 |
3595.3 |
|||
|
42% |
40817 |
15.9 |
5331.5 |
1792 |
7.7 |
24.07 |
4517.4 |
|||
|
45% |
46718 |
19.3 |
6474.9 |
1914 |
7.2 |
27.62 |
5536.0 |
|||
|
48% |
52718 |
23.0 |
7720.3 |
2030 |
6.8 |
31.25 |
6643.3 |
|||
|
51% |
58756 |
27.0 |
9057.8 |
2140 |
6.5 |
34.93 |
7827.4 |
|||
|
54% |
64775 |
31.3 |
10475.5 |
2245 |
6.2 |
38.62 |
9078.8 |
|||
|
57% |
70721 |
35.7 |
11960.0 |
2344 |
5.9 |
42.29 |
10379.3 |
|||
|
60% |
76540 |
40.3 |
13496.2 |
2437 |
5.7 |
45.90 |
11712.7 |
|||
|
63% |
82184 |
45.0 |
15066.5 |
2524 |
5.5 |
49.42 |
13061.5 |
|||
|
66% |
87605 |
49.7 |
16651.2 |
2604 |
5.3 |
52.82 |
14402.1 |
|||
|
69% |
92757 |
54.4 |
18228.5 |
2677 |
5.1 |
56.06 |
15714.7 |
|||
|
72% |
97598 |
59.0 |
19774.6 |
2744 |
4.9 |
59.11 |
16985.4 |
|||
|
75% |
102087 |
63.5 |
21264.1 |
2804 |
4.8 |
61.95 |
18189.1 |
|||
|
78% |
106183 |
67.7 |
22670.8 |
2858 |
4.7 |
64.54 |
19313.5 |
|||
|
81% |
109849 |
71.5 |
23968.0 |
2905 |
4.6 |
66.85 |
20334.3 |
|||
|
84% |
113049 |
75.0 |
25129.8 |
2946 |
4.5 |
68.86 |
21242.4 |
|||
|
87% |
115749 |
78.0 |
26130.9 |
2981 |
4.4 |
70.55 |
22023.2 |
|||
|
100% |
116531 |
78.9 |
26424.7 |
2991 |
4.4 |
71.04 |
22250.4 |
|
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 |
VSC 60x20 |
33% |
24252 |
6.5 |
2613.6 |
1387 |
9.3 |
14.29 |
2074.9 |
89℃ |
|
35% |
27683 |
7.8 |
3128.6 |
1480 |
8.8 |
16.33 |
2530.4 |
|||
|
37% |
31272 |
9.3 |
3705.1 |
1572 |
8.4 |
18.46 |
3038.0 |
|||
|
39% |
34997 |
10.8 |
4339.1 |
1662 |
8.1 |
20.66 |
3595.6 |
|||
|
42% |
40798 |
13.5 |
5388.5 |
1793 |
7.6 |
24.09 |
4523.1 |
|||
|
45% |
46790 |
16.4 |
6544.6 |
1916 |
7.1 |
27.64 |
5546.0 |
|||
|
48% |
52899 |
19.5 |
7796.8 |
2033 |
6.8 |
31.28 |
6659.6 |
|||
|
51% |
59049 |
22.8 |
9137.3 |
2142 |
6.5 |
34.98 |
7845.3 |
|||
|
54% |
65167 |
26.4 |
10559.2 |
2245 |
6.2 |
38.69 |
9095.0 |
|||
|
57% |
71180 |
30.1 |
12053.0 |
2342 |
5.9 |
42.38 |
10392.2 |
|||
|
60% |
77023 |
34.0 |
13604.3 |
2434 |
5.7 |
46.00 |
11722.9 |
|||
|
63% |
82633 |
38.0 |
15191.9 |
2522 |
5.4 |
49.50 |
13072.8 |
|||
|
66% |
87959 |
42.0 |
16788.6 |
2604 |
5.2 |
52.85 |
14411.8 |
|||
|
69% |
92958 |
45.9 |
18362.6 |
2679 |
5.1 |
56.01 |
15712.8 |
|||
|
72% |
97596 |
49.7 |
19881.7 |
2747 |
4.9 |
58.95 |
16955.4 |
|||
|
75% |
101855 |
53.3 |
21317.1 |
2807 |
4.8 |
61.63 |
18115.8 |
|||
|
78% |
105731 |
56.6 |
22646.8 |
2858 |
4.7 |
64.07 |
19173.3 |
|||
|
81% |
109236 |
59.6 |
23858.5 |
2901 |
4.6 |
66.25 |
20125.1 |
|||
|
84% |
112399 |
62.4 |
24951.0 |
2935 |
4.5 |
68.20 |
20961.0 |
|||
|
87% |
115272 |
64.8 |
25934.1 |
2962 |
4.4 |
69.96 |
21697.3 |
|||
|
100% |
116176 |
65.6 |
26240.6 |
2970 |
4.4 |
70.50 |
21926.1 |
|
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 |
USC 54x23 |
33% |
22163 |
7.6 |
2532.7 |
1487 |
8.8 |
12.90 |
2009.3 |
90℃ |
|
35% |
25389 |
9.1 |
3046.0 |
1589 |
8.3 |
14.79 |
2461.3 |
|||
|
37% |
28798 |
10.8 |
3625.0 |
1691 |
7.9 |
16.80 |
2974.5 |
|||
|
39% |
32358 |
12.7 |
4266.6 |
1790 |
7.6 |
18.90 |
3543.3 |
|||
|
42% |
37913 |
15.9 |
5337.2 |
1934 |
7.1 |
22.21 |
4498.1 |
|||
|
45% |
43650 |
19.5 |
6525.9 |
2070 |
6.7 |
25.65 |
5560.2 |
|||
|
48% |
49496 |
23.3 |
7819.8 |
2198 |
6.3 |
29.18 |
6716.2 |
|||
|
51% |
55388 |
27.5 |
9208.1 |
2318 |
6.0 |
32.76 |
7951.5 |
|||
|
54% |
61275 |
31.9 |
10680.7 |
2431 |
5.7 |
36.36 |
9254.5 |
|||
|
56% |
65173 |
34.9 |
11704.4 |
2503 |
5.6 |
38.75 |
10155.6 |
|||
|
60% |
72850 |
41.3 |
13838.0 |
2638 |
5.3 |
43.48 |
12011.8 |
|||
|
63% |
78456 |
46.3 |
15497.4 |
2732 |
5.1 |
46.97 |
13436.0 |
|||
|
66% |
83886 |
51.3 |
17187.6 |
2820 |
4.9 |
50.36 |
14870.5 |
|||
|
69% |
89094 |
56.4 |
18884.7 |
2901 |
4.7 |
53.63 |
16292.4 |
|||
|
72% |
94030 |
61.4 |
20559.0 |
2975 |
4.6 |
56.76 |
17681.0 |
|||
|
75% |
98634 |
66.2 |
22174.3 |
3041 |
4.4 |
59.69 |
19007.4 |
|||
|
78% |
102836 |
70.7 |
23688.3 |
3098 |
4.3 |
62.39 |
20238.0 |
|||
|
81% |
106549 |
74.8 |
25053.6 |
3145 |
4.3 |
64.79 |
21335.0 |
|||
|
84% |
109674 |
78.3 |
26218.3 |
3183 |
4.2 |
66.82 |
22269.9 |
|||
|
87% |
112092 |
81.0 |
27126.4 |
3211 |
4.1 |
68.40 |
22997.1 |
|||
|
100% |
112716 |
81.7 |
27361.9 |
3218 |
4.1 |
68.81 |
23185.3 |
|
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 |
USC 54x23 |
33% |
22233 |
6.4 |
2577.3 |
1487 |
8.6 |
12.93 |
2013.1 |
92℃ |
|
35% |
25510 |
7.7 |
3096.2 |
1590 |
8.2 |
14.84 |
2470.4 |
|||
|
37% |
28943 |
9.2 |
3684.7 |
1691 |
7.9 |
16.86 |
2986.1 |
|||
|
39% |
32504 |
10.8 |
4336.8 |
1790 |
7.5 |
18.99 |
3558.5 |
|||
|
42% |
38033 |
13.6 |
5420.3 |
1933 |
7.0 |
22.30 |
4513.3 |
|||
|
45% |
43720 |
16.5 |
6613.4 |
2069 |
6.6 |
25.72 |
5571.5 |
|||
|
48% |
49499 |
19.8 |
7901.9 |
2197 |
6.3 |
29.20 |
6716.5 |
|||
|
51% |
55312 |
23.2 |
9276.3 |
2318 |
6.0 |
32.70 |
7937.8 |
|||
|
54% |
61107 |
26.8 |
10731.0 |
2431 |
5.7 |
36.22 |
9219.9 |
|||
|
56% |
64937 |
29.4 |
11743.1 |
2503 |
5.5 |
38.56 |
10106.8 |
|||
|
60% |
72465 |
34.6 |
13859.7 |
2638 |
5.2 |
43.22 |
11938.9 |
|||
|
63% |
77950 |
38.8 |
15515.2 |
2732 |
5.0 |
46.67 |
13351.7 |
|||
|
66% |
83258 |
43.0 |
17209.8 |
2820 |
4.8 |
50.06 |
14782.0 |
|||
|
69% |
88357 |
47.3 |
18919.3 |
2901 |
4.7 |
53.35 |
16205.9 |
|||
|
72% |
93213 |
51.5 |
20613.1 |
2974 |
4.5 |
56.50 |
17594.8 |
|||
|
75% |
97792 |
55.6 |
22256.4 |
3040 |
4.4 |
59.47 |
18929.3 |
|||
|
78% |
102057 |
59.5 |
23812.3 |
3097 |
4.3 |
62.20 |
20170.6 |
|||
|
81% |
105970 |
63.1 |
25244.6 |
3145 |
4.2 |
64.65 |
21292.0 |
|||
|
84% |
109488 |
66.3 |
26520.7 |
3185 |
4.1 |
66.80 |
22276.8 |
|||
|
87% |
112562 |
69.0 |
27614.1 |
3216 |
4.1 |
68.59 |
23099.2 |
|||
|
100% |
113479 |
69.8 |
27934.3 |
3224 |
4.1 |
69.11 |
23332.2 |
Support
Manuals & Documents
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