|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Speed(RPM) |
Efficiency(g/W) |
Torque(N·m) |
Power Output(W) |
Temperature（℃） |
|---|---|---|---|---|---|---|---|---|---|---|
|
88V(24S LiPo) |
28x13 |
35% |
5509 |
8.9 |
786.1 |
2741 |
7.0 |
1.91 |
548.8 |
/ |
|
37% |
6125 |
10.2 |
896.3 |
2888 |
6.8 |
2.13 |
643.7 |
|||
|
39% |
6797 |
11.6 |
1016.9 |
3038 |
6.7 |
2.36 |
751.4 |
|||
|
42% |
7871 |
13.8 |
1215.0 |
3263 |
6.5 |
2.73 |
932.8 |
|||
|
45% |
8991 |
16.3 |
1432.7 |
3480 |
6.3 |
3.11 |
1134.5 |
|||
|
48% |
10136 |
19.0 |
1670.3 |
3686 |
6.1 |
3.51 |
1354.4 |
|||
|
51% |
11296 |
21.9 |
1928.7 |
3883 |
5.9 |
3.92 |
1591.9 |
|||
|
54% |
12474 |
25.1 |
2209.9 |
4072 |
5.6 |
4.34 |
1848.8 |
|||
|
57% |
13683 |
28.6 |
2516.6 |
4257 |
5.4 |
4.77 |
2128.1 |
|||
|
60% |
14939 |
32.4 |
2852.7 |
4440 |
5.2 |
5.24 |
2434.3 |
|||
|
63% |
16260 |
36.6 |
3222.1 |
4626 |
5.0 |
5.72 |
2772.5 |
|||
|
66% |
17666 |
41.2 |
3628.5 |
4814 |
4.9 |
6.24 |
3147.4 |
|||
|
69% |
19169 |
46.3 |
4073.8 |
5006 |
4.7 |
6.80 |
3562.2 |
|||
|
72% |
20779 |
51.8 |
4558.8 |
5199 |
4.6 |
7.38 |
4017.7 |
|||
|
75% |
22492 |
57.8 |
5084.2 |
5392 |
4.4 |
7.99 |
4512.9 |
|||
|
78% |
24294 |
64.2 |
5654.6 |
5581 |
4.3 |
8.64 |
5046.8 |
|||
|
81% |
26154 |
71.4 |
6283.1 |
5765 |
4.2 |
9.32 |
5624.2 |
|||
|
84% |
28021 |
79.5 |
6993.8 |
5945 |
4.0 |
10.06 |
6259.4 |
|||
|
87% |
29824 |
88.8 |
7811.9 |
6124 |
3.8 |
10.87 |
6973.7 |
|||
|
90% |
31467 |
99.2 |
8734.5 |
6305 |
3.6 |
11.77 |
7773.1 |
|||
|
100% |
34029 |
121.6 |
10701.1 |
6662 |
3.2 |
13.64 |
9517.4 |
-
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
-
- Fixed-Wing UAV Cruise Motor Convenient, efficient and stable.
- 62XX
- 72XX
- 80XX
- 100XX
-
-
- PROPELLER Carbon Plastic Propeller
- Carbon Plastic Propeller
-
-
RC Power Systems
- e-Vehicle Power Systems
- Service and Support
vertical take-off and landing (VTOL) drones.
Meant to seamlessly replace 130CC combustion engines.
29-inch propellers
a maximum thrust of
39kg at 92V
across diverse flight conditions.
rectangular exhaust outlet with
a centrifugal fan design,
reducing airflow resistance and
turbulence, enhancing heat
exhaust efficiency.
operation even in high-load flight
conditions.
Superior Reliability
upper and
lower steel
mesh structure
particles ≥1mm
in diameter
flight environments
such as dust and rain
- IPC Sensor
Optional - IPC Propeller
Positioning - Boss Clearance
Design - Multi-propeller
Compatibility
allowing for flexible selection.
minimize the risk of colliding with the ground.
edge structure of propeller roots, accommodating both non-folding and folding propellers.
diverse applications.
Design for a Safer Flight
- Knurled Shaft
- Knurled shaft-to-bracket interface with side set screw locking for dual redundant security.
- Multi-Layer Securing Mechanism
- Multi-layer securing mechanism at the rotor shaft end, utilizing copper washer, circlip, and screw fastening for enhanced stability and reliability.
- Triple-Bearing System
- The triple-bearing system with precision dynamic balancing, enhancing impact resistance and durability for worry-free flight operations.
- Silicon Steel and Enameled Wires
- It is designed with industry-leading 0.2mm low-loss silicon steel cores and high-grade 240°C temperature-resistant enameled wires.
- Magnet Segment
- The high-grade, strong magnetic arc-shaped magnets enhance the magnetic energy density, delivering powerful torque for the motor. This meets large-thrust needs during climbing, while maintaining high efficiency during cruise, improving cruise flight efficiency by 2-4% compared to motors of similar grades.
- Silicone Rubber Cable Sleeves
- The motor’s three-phase wire outlet comes with a custom silicone rubber cable sleeve, combining aesthetic appeal with superior insulation.
Optimized Design
The newly designed magnetic circuit highly matches the driving parameter requirements,
ensuring a more rapid propulsion output response.
1000+ Hour Testing
Rigorous suite of industrial tests (compatibility, waterproof, salt spray, stress,combined env/vibration, long-term
fatigue) ensures the motor maintains peak performance and reliability throughout its extended lifecycle.
-
- Model
- Protection level
- Motor Size
- Slot& Pole
- Dynamic balance
- Bearing
- Enamelled wire
- Motor axle diameter
- Magnet
- Props mounting dimensions
- Isolation test
- Motor mounting dimensions
- Rated power input
- Rated power output
- Stator process
-
- C10040-90KV
- IPX5
- Φ110*H98.2 mm
- 24N28P
- ≤25 mg
- Water proof bearing
- 240 ℃
- Φ12 mm
- 140 ℃
- 6×M5@D29 mm & 6×M5@D30 mm
- 1000V AC high voltage resistance test
- 4×M6@D55 mm
- 2520 W
- 2130 W
- High standard silicon steel sheet, rust proof, 180℃ high temperature resistance paint-coat
-
- KV
- Battery(LiPo)
- No-load current
- Maximum current (non-hermetic ambient temperature ≤ 25℃）
- Rated thrust
- Max thrust
- Resistance
- Wire Size
- Three-phase wires length
- Magnetic encoder cable length
- Weight（with wires）
-
- 90 KV
- LiPo-24S (92V)
- ≤7.9 A
- 144 A
- 12~14 kg (92V@29x12)
- 39 kg (92V@29x12)
- 10.46~11.11 mΩ
- enameled wire direct lead-out
- 100mm
- 130mm
- 2044 g
-
- Motor
- Propeller
- ESC
- Battery
- Takeoff weight of Single motor
-
- C10040-90KV
- 28x13/29x12
- XRotor Pro H300A 24S BLDC IPC G3
- 24S LiPo
- 60~65kg
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Speed(RPM) |
Efficiency(g/W) |
Torque(N·m) |
Power Output(W) |
Temperature（℃） |
|---|---|---|---|---|---|---|---|---|---|---|
|
92V(24S LiPo) |
28x13 |
35% |
5938 |
9.5 |
872.8 |
2850 |
6.8 |
2.07 |
617.2 |
88℃ |
|
37% |
6591 |
10.8 |
997.2 |
3002 |
6.6 |
2.30 |
723.7 |
|||
|
39% |
7327 |
12.3 |
1135.3 |
3162 |
6.5 |
2.56 |
847.7 |
|||
|
42% |
8529 |
14.8 |
1363.3 |
3403 |
6.3 |
2.97 |
1059.1 |
|||
|
45% |
9790 |
17.6 |
1614.7 |
3634 |
6.1 |
3.40 |
1294.7 |
|||
|
48% |
11069 |
20.5 |
1889.5 |
3851 |
5.9 |
3.84 |
1549.9 |
|||
|
51% |
12345 |
23.8 |
2187.5 |
4055 |
5.6 |
4.29 |
1822.7 |
|||
|
54% |
13617 |
27.3 |
2508.4 |
4249 |
5.4 |
4.75 |
2113.2 |
|||
|
57% |
14894 |
31.0 |
2853.6 |
4437 |
5.2 |
5.22 |
2423.9 |
|||
|
60% |
16196 |
35.1 |
3225.9 |
4622 |
5.0 |
5.70 |
2759.2 |
|||
|
63% |
17548 |
39.4 |
3629.6 |
4808 |
4.8 |
6.21 |
3125.0 |
|||
|
66% |
18977 |
44.2 |
4069.1 |
4996 |
4.7 |
6.74 |
3527.3 |
|||
|
69% |
20506 |
49.4 |
4548.0 |
5189 |
4.5 |
7.31 |
3970.9 |
|||
|
72% |
22150 |
55.1 |
5068.4 |
5385 |
4.4 |
7.91 |
4458.1 |
|||
|
75% |
23914 |
61.2 |
5633.6 |
5579 |
4.2 |
8.54 |
4989.4 |
|||
|
78% |
25787 |
68.0 |
6253.3 |
5770 |
4.1 |
9.21 |
5566.9 |
|||
|
81% |
27738 |
75.6 |
6952.9 |
5955 |
4.0 |
9.95 |
6203.1 |
|||
|
84% |
29715 |
84.5 |
7778.2 |
6137 |
3.8 |
10.78 |
6929.0 |
|||
|
87% |
31636 |
95.5 |
8783.0 |
6325 |
3.6 |
11.77 |
7792.1 |
|||
|
90% |
33387 |
108.4 |
9978.0 |
6526 |
3.3 |
12.91 |
8819.5 |
|||
|
100% |
35963 |
135.8 |
12493.2 |
6932 |
2.9 |
15.26 |
11074.2 |
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Speed(RPM) |
Efficiency(g/W) |
Torque(N·m) |
Power Output(W) |
Temperature（℃） |
|---|---|---|---|---|---|---|---|---|---|---|
|
88V(24S LiPo) |
29x12 |
35% |
6010 |
9.4 |
826.6 |
2724 |
7.3 |
2.08 |
593.1 |
/ |
|
37% |
6676 |
10.7 |
941.9 |
2870 |
7.1 |
2.31 |
695.0 |
|||
|
39% |
7401 |
12.2 |
1071.5 |
3020 |
6.9 |
2.57 |
811.6 |
|||
|
42% |
8560 |
14.6 |
1289.2 |
3244 |
6.6 |
2.97 |
1009.8 |
|||
|
45% |
9772 |
17.4 |
1531.0 |
3461 |
6.4 |
3.40 |
1231.8 |
|||
|
48% |
11013 |
20.4 |
1794.6 |
3667 |
6.1 |
3.84 |
1474.0 |
|||
|
51% |
12276 |
23.6 |
2079.2 |
3862 |
5.9 |
4.29 |
1735.0 |
|||
|
54% |
13563 |
27.1 |
2385.8 |
4050 |
5.7 |
4.75 |
2015.7 |
|||
|
57% |
14885 |
30.9 |
2717.3 |
4233 |
5.5 |
5.23 |
2318.9 |
|||
|
60% |
16259 |
35.0 |
3078.2 |
4414 |
5.3 |
5.73 |
2649.3 |
|||
|
63% |
17704 |
39.5 |
3474.2 |
4595 |
5.1 |
6.26 |
3012.8 |
|||
|
66% |
19238 |
44.4 |
3911.4 |
4779 |
4.9 |
6.83 |
3415.5 |
|||
|
69% |
20877 |
49.9 |
4395.4 |
4966 |
4.7 |
7.43 |
3863.4 |
|||
|
72% |
22630 |
56.0 |
4931.1 |
5156 |
4.6 |
8.08 |
4361.0 |
|||
|
75% |
24497 |
62.7 |
5522.3 |
5348 |
4.4 |
8.77 |
4910.6 |
|||
|
78% |
26466 |
70.1 |
6172.1 |
5538 |
4.3 |
9.51 |
5512.1 |
|||
|
81% |
28509 |
78.2 |
6883.9 |
5723 |
4.1 |
10.28 |
6163.7 |
|||
|
84% |
30580 |
87.0 |
7661.1 |
5901 |
4.0 |
11.11 |
6862.6 |
|||
|
87% |
32613 |
96.6 |
8502.5 |
6071 |
3.8 |
11.96 |
7603.9 |
|||
|
90% |
34519 |
106.7 |
9391.1 |
6230 |
3.7 |
12.84 |
8373.5 |
|||
|
100% |
38210 |
131.0 |
11532.4 |
6576 |
3.3 |
14.84 |
10220.3 |
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Speed(RPM) |
Efficiency(g/W) |
Torque(N·m) |
Power Output(W) |
Temperature（℃） |
|---|---|---|---|---|---|---|---|---|---|---|
|
92V (24S LiPo) |
29x12 |
35% |
6553 |
10.0 |
924.0 |
2844 |
7.1 |
2.27 |
676.0 |
99℃ |
|
37% |
7276 |
11.4 |
1053.0 |
2991 |
6.9 |
2.52 |
790.3 |
|||
|
39% |
8060 |
13.0 |
1197.5 |
3144 |
6.7 |
2.80 |
920.4 |
|||
|
42% |
9318 |
15.7 |
1440.9 |
3374 |
6.5 |
3.23 |
1141.7 |
|||
|
45% |
10642 |
18.6 |
1714.1 |
3600 |
6.2 |
3.69 |
1391.3 |
|||
|
48% |
12011 |
21.9 |
2015.8 |
3818 |
6.0 |
4.17 |
1666.7 |
|||
|
51% |
13415 |
25.5 |
2345.7 |
4026 |
5.7 |
4.67 |
1967.1 |
|||
|
54% |
14857 |
29.4 |
2704.3 |
4227 |
5.5 |
5.18 |
2293.3 |
|||
|
57% |
16343 |
33.6 |
3093.4 |
4421 |
5.3 |
5.72 |
2647.6 |
|||
|
60% |
17888 |
38.2 |
3515.5 |
4610 |
5.1 |
6.28 |
3033.0 |
|||
|
63% |
19504 |
43.2 |
3973.8 |
4797 |
4.9 |
6.88 |
3453.3 |
|||
|
66% |
21206 |
48.6 |
4471.4 |
4981 |
4.7 |
7.50 |
3912.0 |
|||
|
69% |
23003 |
54.5 |
5011.7 |
5166 |
4.6 |
8.16 |
4412.1 |
|||
|
72% |
24897 |
60.8 |
5598.5 |
5349 |
4.4 |
8.85 |
4955.9 |
|||
|
75% |
26883 |
67.8 |
6238.7 |
5532 |
4.3 |
9.57 |
5546.3 |
|||
|
78% |
28942 |
75.5 |
6943.7 |
5715 |
4.2 |
10.34 |
6188.9 |
|||
|
81% |
31040 |
84.0 |
7732.2 |
5898 |
4.0 |
11.16 |
6894.1 |
|||
|
84% |
33127 |
93.8 |
8626.5 |
6084 |
3.8 |
12.05 |
7677.5 |
|||
|
87% |
35131 |
104.8 |
9640.8 |
6271 |
3.6 |
13.02 |
8552.3 |
|||
|
90% |
36957 |
116.9 |
10753.3 |
6458 |
3.4 |
14.06 |
9507.9 |
|||
|
100% |
39266 |
136.0 |
12517.5 |
6728 |
3.1 |
15.67 |
11041.3 |
Support
Manuals & Documents
Disclaimer
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vertical take-off and landing (VTOL) drones.
Meant to seamlessly replace 130CC combustion engines.
29-inch propellers
a maximum thrust of
39kg at 92V
across diverse flight conditions.
rectangular exhaust outlet with
a centrifugal fan design,
reducing airflow resistance and
turbulence, enhancing heat
exhaust efficiency.
operation even in high-load flight
conditions.
Superior Reliability
upper and
lower steel
mesh structure
particles ≥1mm
in diameter
flight environments
such as dust and rain
- IPC Sensor
Optional - IPC Propeller
Positioning - Boss Clearance
Design - Multi-propeller
Compatibility
allowing for flexible selection.
minimize the risk of colliding with the ground.
edge structure of propeller roots, accommodating both non-folding and folding propellers.
diverse applications.
Design for a Safer Flight
- Knurled Shaft
- Knurled shaft-to-bracket interface with side set screw locking for dual redundant security.
- Multi-Layer Securing Mechanism
- Multi-layer securing mechanism at the rotor shaft end, utilizing copper washer, circlip, and screw fastening for enhanced stability and reliability.
- Triple-Bearing System
- The triple-bearing system with precision dynamic balancing, enhancing impact resistance and durability for worry-free flight operations.
- Silicon Steel and Enameled Wires
- It is designed with industry-leading 0.2mm low-loss silicon steel cores and high-grade 240°C temperature-resistant enameled wires.
- Magnet Segment
- The high-grade, strong magnetic arc-shaped magnets enhance the magnetic energy density, delivering powerful torque for the motor. This meets large-thrust needs during climbing, while maintaining high efficiency during cruise, improving cruise flight efficiency by 2-4% compared to motors of similar grades.
- Silicone Rubber Cable Sleeves
- The motor’s three-phase wire outlet comes with a custom silicone rubber cable sleeve, combining aesthetic appeal with superior insulation.
Optimized Design
The newly designed magnetic circuit highly matches the driving parameter requirements,
ensuring a more rapid propulsion output response.
1000+ Hour Testing
Rigorous suite of industrial tests (compatibility, waterproof, salt spray, stress,combined env/vibration, long-term
fatigue) ensures the motor maintains peak performance and reliability throughout its extended lifecycle.
-
- Model
- Protection level
- Motor Size
- Slot& Pole
- Dynamic balance
- Bearing
- Enamelled wire
- Motor axle diameter
- Magnet
- Props mounting dimensions
- Isolation test
- Motor mounting dimensions
- Rated power input
- Rated power output
- Stator process
-
- C10040-90KV
- IPX5
- Φ110*H98.2 mm
- 24N28P
- ≤25 mg
- Water proof bearing
- 240 ℃
- Φ12 mm
- 140 ℃
- 6×M5@D29 mm & 6×M5@D30 mm
- 1000V AC high voltage resistance test
- 4×M6@D55 mm
- 2520 W
- 2130 W
- High standard silicon steel sheet, rust proof, 180℃ high temperature resistance paint-coat
-
- KV
- Battery(LiPo)
- No-load current
- Maximum current (non-hermetic ambient temperature ≤ 25℃）
- Rated thrust
- Max thrust
- Resistance
- Wire Size
- Three-phase wires length
- Magnetic encoder cable length
- Weight（with wires）
-
- 90 KV
- LiPo-24S (92V)
- ≤7.9 A
- 144 A
- 12~14 kg (92V@29x12)
- 39 kg (92V@29x12)
- 10.46~11.11 mΩ
- enameled wire direct lead-out
- 100mm
- 130mm
- 2044 g
-
- Motor
- Propeller
- ESC
- Battery
- Takeoff weight of Single motor
-
- C10040-90KV
- 28x13/29x12
- XRotor Pro H300A 24S BLDC IPC G3
- 24S LiPo
- 60~65kg
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Speed(RPM) |
Efficiency(g/W) |
Torque(N·m) |
Power Output(W) |
Temperature（℃） |
|---|---|---|---|---|---|---|---|---|---|---|
|
88V(24S LiPo) |
28x13 |
35% |
5509 |
8.9 |
786.1 |
2741 |
7.0 |
1.91 |
548.8 |
/ |
|
37% |
6125 |
10.2 |
896.3 |
2888 |
6.8 |
2.13 |
643.7 |
|||
|
39% |
6797 |
11.6 |
1016.9 |
3038 |
6.7 |
2.36 |
751.4 |
|||
|
42% |
7871 |
13.8 |
1215.0 |
3263 |
6.5 |
2.73 |
932.8 |
|||
|
45% |
8991 |
16.3 |
1432.7 |
3480 |
6.3 |
3.11 |
1134.5 |
|||
|
48% |
10136 |
19.0 |
1670.3 |
3686 |
6.1 |
3.51 |
1354.4 |
|||
|
51% |
11296 |
21.9 |
1928.7 |
3883 |
5.9 |
3.92 |
1591.9 |
|||
|
54% |
12474 |
25.1 |
2209.9 |
4072 |
5.6 |
4.34 |
1848.8 |
|||
|
57% |
13683 |
28.6 |
2516.6 |
4257 |
5.4 |
4.77 |
2128.1 |
|||
|
60% |
14939 |
32.4 |
2852.7 |
4440 |
5.2 |
5.24 |
2434.3 |
|||
|
63% |
16260 |
36.6 |
3222.1 |
4626 |
5.0 |
5.72 |
2772.5 |
|||
|
66% |
17666 |
41.2 |
3628.5 |
4814 |
4.9 |
6.24 |
3147.4 |
|||
|
69% |
19169 |
46.3 |
4073.8 |
5006 |
4.7 |
6.80 |
3562.2 |
|||
|
72% |
20779 |
51.8 |
4558.8 |
5199 |
4.6 |
7.38 |
4017.7 |
|||
|
75% |
22492 |
57.8 |
5084.2 |
5392 |
4.4 |
7.99 |
4512.9 |
|||
|
78% |
24294 |
64.2 |
5654.6 |
5581 |
4.3 |
8.64 |
5046.8 |
|||
|
81% |
26154 |
71.4 |
6283.1 |
5765 |
4.2 |
9.32 |
5624.2 |
|||
|
84% |
28021 |
79.5 |
6993.8 |
5945 |
4.0 |
10.06 |
6259.4 |
|||
|
87% |
29824 |
88.8 |
7811.9 |
6124 |
3.8 |
10.87 |
6973.7 |
|||
|
90% |
31467 |
99.2 |
8734.5 |
6305 |
3.6 |
11.77 |
7773.1 |
|||
|
100% |
34029 |
121.6 |
10701.1 |
6662 |
3.2 |
13.64 |
9517.4 |
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Speed(RPM) |
Efficiency(g/W) |
Torque(N·m) |
Power Output(W) |
Temperature（℃） |
|---|---|---|---|---|---|---|---|---|---|---|
|
92V(24S LiPo) |
28x13 |
35% |
5938 |
9.5 |
872.8 |
2850 |
6.8 |
2.07 |
617.2 |
88℃ |
|
37% |
6591 |
10.8 |
997.2 |
3002 |
6.6 |
2.30 |
723.7 |
|||
|
39% |
7327 |
12.3 |
1135.3 |
3162 |
6.5 |
2.56 |
847.7 |
|||
|
42% |
8529 |
14.8 |
1363.3 |
3403 |
6.3 |
2.97 |
1059.1 |
|||
|
45% |
9790 |
17.6 |
1614.7 |
3634 |
6.1 |
3.40 |
1294.7 |
|||
|
48% |
11069 |
20.5 |
1889.5 |
3851 |
5.9 |
3.84 |
1549.9 |
|||
|
51% |
12345 |
23.8 |
2187.5 |
4055 |
5.6 |
4.29 |
1822.7 |
|||
|
54% |
13617 |
27.3 |
2508.4 |
4249 |
5.4 |
4.75 |
2113.2 |
|||
|
57% |
14894 |
31.0 |
2853.6 |
4437 |
5.2 |
5.22 |
2423.9 |
|||
|
60% |
16196 |
35.1 |
3225.9 |
4622 |
5.0 |
5.70 |
2759.2 |
|||
|
63% |
17548 |
39.4 |
3629.6 |
4808 |
4.8 |
6.21 |
3125.0 |
|||
|
66% |
18977 |
44.2 |
4069.1 |
4996 |
4.7 |
6.74 |
3527.3 |
|||
|
69% |
20506 |
49.4 |
4548.0 |
5189 |
4.5 |
7.31 |
3970.9 |
|||
|
72% |
22150 |
55.1 |
5068.4 |
5385 |
4.4 |
7.91 |
4458.1 |
|||
|
75% |
23914 |
61.2 |
5633.6 |
5579 |
4.2 |
8.54 |
4989.4 |
|||
|
78% |
25787 |
68.0 |
6253.3 |
5770 |
4.1 |
9.21 |
5566.9 |
|||
|
81% |
27738 |
75.6 |
6952.9 |
5955 |
4.0 |
9.95 |
6203.1 |
|||
|
84% |
29715 |
84.5 |
7778.2 |
6137 |
3.8 |
10.78 |
6929.0 |
|||
|
87% |
31636 |
95.5 |
8783.0 |
6325 |
3.6 |
11.77 |
7792.1 |
|||
|
90% |
33387 |
108.4 |
9978.0 |
6526 |
3.3 |
12.91 |
8819.5 |
|||
|
100% |
35963 |
135.8 |
12493.2 |
6932 |
2.9 |
15.26 |
11074.2 |
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Speed(RPM) |
Efficiency(g/W) |
Torque(N·m) |
Power Output(W) |
Temperature（℃） |
|---|---|---|---|---|---|---|---|---|---|---|
|
88V(24S LiPo) |
29x12 |
35% |
6010 |
9.4 |
826.6 |
2724 |
7.3 |
2.08 |
593.1 |
/ |
|
37% |
6676 |
10.7 |
941.9 |
2870 |
7.1 |
2.31 |
695.0 |
|||
|
39% |
7401 |
12.2 |
1071.5 |
3020 |
6.9 |
2.57 |
811.6 |
|||
|
42% |
8560 |
14.6 |
1289.2 |
3244 |
6.6 |
2.97 |
1009.8 |
|||
|
45% |
9772 |
17.4 |
1531.0 |
3461 |
6.4 |
3.40 |
1231.8 |
|||
|
48% |
11013 |
20.4 |
1794.6 |
3667 |
6.1 |
3.84 |
1474.0 |
|||
|
51% |
12276 |
23.6 |
2079.2 |
3862 |
5.9 |
4.29 |
1735.0 |
|||
|
54% |
13563 |
27.1 |
2385.8 |
4050 |
5.7 |
4.75 |
2015.7 |
|||
|
57% |
14885 |
30.9 |
2717.3 |
4233 |
5.5 |
5.23 |
2318.9 |
|||
|
60% |
16259 |
35.0 |
3078.2 |
4414 |
5.3 |
5.73 |
2649.3 |
|||
|
63% |
17704 |
39.5 |
3474.2 |
4595 |
5.1 |
6.26 |
3012.8 |
|||
|
66% |
19238 |
44.4 |
3911.4 |
4779 |
4.9 |
6.83 |
3415.5 |
|||
|
69% |
20877 |
49.9 |
4395.4 |
4966 |
4.7 |
7.43 |
3863.4 |
|||
|
72% |
22630 |
56.0 |
4931.1 |
5156 |
4.6 |
8.08 |
4361.0 |
|||
|
75% |
24497 |
62.7 |
5522.3 |
5348 |
4.4 |
8.77 |
4910.6 |
|||
|
78% |
26466 |
70.1 |
6172.1 |
5538 |
4.3 |
9.51 |
5512.1 |
|||
|
81% |
28509 |
78.2 |
6883.9 |
5723 |
4.1 |
10.28 |
6163.7 |
|||
|
84% |
30580 |
87.0 |
7661.1 |
5901 |
4.0 |
11.11 |
6862.6 |
|||
|
87% |
32613 |
96.6 |
8502.5 |
6071 |
3.8 |
11.96 |
7603.9 |
|||
|
90% |
34519 |
106.7 |
9391.1 |
6230 |
3.7 |
12.84 |
8373.5 |
|||
|
100% |
38210 |
131.0 |
11532.4 |
6576 |
3.3 |
14.84 |
10220.3 |
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Speed(RPM) |
Efficiency(g/W) |
Torque(N·m) |
Power Output(W) |
Temperature（℃） |
|---|---|---|---|---|---|---|---|---|---|---|
|
92V (24S LiPo) |
29x12 |
35% |
6553 |
10.0 |
924.0 |
2844 |
7.1 |
2.27 |
676.0 |
99℃ |
|
37% |
7276 |
11.4 |
1053.0 |
2991 |
6.9 |
2.52 |
790.3 |
|||
|
39% |
8060 |
13.0 |
1197.5 |
3144 |
6.7 |
2.80 |
920.4 |
|||
|
42% |
9318 |
15.7 |
1440.9 |
3374 |
6.5 |
3.23 |
1141.7 |
|||
|
45% |
10642 |
18.6 |
1714.1 |
3600 |
6.2 |
3.69 |
1391.3 |
|||
|
48% |
12011 |
21.9 |
2015.8 |
3818 |
6.0 |
4.17 |
1666.7 |
|||
|
51% |
13415 |
25.5 |
2345.7 |
4026 |
5.7 |
4.67 |
1967.1 |
|||
|
54% |
14857 |
29.4 |
2704.3 |
4227 |
5.5 |
5.18 |
2293.3 |
|||
|
57% |
16343 |
33.6 |
3093.4 |
4421 |
5.3 |
5.72 |
2647.6 |
|||
|
60% |
17888 |
38.2 |
3515.5 |
4610 |
5.1 |
6.28 |
3033.0 |
|||
|
63% |
19504 |
43.2 |
3973.8 |
4797 |
4.9 |
6.88 |
3453.3 |
|||
|
66% |
21206 |
48.6 |
4471.4 |
4981 |
4.7 |
7.50 |
3912.0 |
|||
|
69% |
23003 |
54.5 |
5011.7 |
5166 |
4.6 |
8.16 |
4412.1 |
|||
|
72% |
24897 |
60.8 |
5598.5 |
5349 |
4.4 |
8.85 |
4955.9 |
|||
|
75% |
26883 |
67.8 |
6238.7 |
5532 |
4.3 |
9.57 |
5546.3 |
|||
|
78% |
28942 |
75.5 |
6943.7 |
5715 |
4.2 |
10.34 |
6188.9 |
|||
|
81% |
31040 |
84.0 |
7732.2 |
5898 |
4.0 |
11.16 |
6894.1 |
|||
|
84% |
33127 |
93.8 |
8626.5 |
6084 |
3.8 |
12.05 |
7677.5 |
|||
|
87% |
35131 |
104.8 |
9640.8 |
6271 |
3.6 |
13.02 |
8552.3 |
|||
|
90% |
36957 |
116.9 |
10753.3 |
6458 |
3.4 |
14.06 |
9507.9 |
|||
|
100% |
39266 |
136.0 |
12517.5 |
6728 |
3.1 |
15.67 |
11041.3 |
Support
Manuals & Documents
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