HOBBYWING: UAV Propulsion Systems, RC Motors & ESCs, e-Vehicle Power System
Hobbywing C6225 Fixed Wing Motor
C6225
Universally Versatile Propulsion
Perfectly suited for both fixed-wing cruise and vertical take-off and landing (VTOL) drones
Efficient Cooling with Great Power
Drone Propeller Motor
Paired with
21-inch propellers
the motor delivers up to
a maximum thrust of
14.8kg at 48V
easily handling the dynamic thrust
needs during rapid maneuvers and
sudden payload changes
Efficient Heat Dissipation C6225 Fixed Wing Motor 220kv
Optimized rectangular outlet and
centrifugal fan design reduce
resistance and turbulence,
dramatically improving
heat dissipation
The motor dissipation efficiency improves by 20%
The winding temperature rise is
significantly reduced compared
tomotors of other brands with
similar specifications, ensuring
stable and long-term operation
even in high-load flight conditions
High Protection,
Superior Reliability
High Protection Drone Electric Motor
The motor is designed with
upper and
lower steel
mesh structure

Effectively prevents
ingress of particles
1 mm and larger
in diameter.

Adapts to harsh
flight environments
such as dust and rain
Flexible Choice,
Convenient Application
Intelligent Propeller Control Component Of Uav Motor
  • The stator base is compatible with an IPC
  • (Intelligent Propeller Control) component,
  • allowing for flexible selection.
Paired With An Ipc Esc
  • Paired with an IPC ESC, users can customize
  • the propeller stopping position to minimize
  • the risk of colliding with the ground.
Rotor Bracket
  • The rotor bracket adopts a boss clearance design that effectively prevents
  • interference with the propeller root edge structure, ensuring seamless compatibility
  • and secure installation for both non-folding and folding propellers.
Drone Motor With Propeller eVTOL Motor
  • Supports multiple mounting configurations
  • for quick adaptation, to meet the demands of diverse applications.
Superior Material and
Design for a Safer Flight
Anti Loosening Design
Anti-Loosening Design
The rotor shaft end is fixed by copper washers, circlips, and screws to enhance motor reliability.
Triple Bearing Architecture
Triple-Bearing
Architecture
The triple-bearing architecture optimizes dynamic balance, enhancing impact resistance and durability of the motor to ensure safe flights.
Silicon Steel And Enameled Wires
Silicon Steel and
Enameled Wires
t is designed with industry-leading 0.2mm low-loss silicon steel cores and high-grade 220°C temperature-resistant enameled wires.
Magnet Segment
Magnet Segment
High-grade, strong magnetic arc-shaped magnets boost magnetic energy density for superior torque during climbs and heavy lifts. Cruise efficiency gains of 2–4% over comparable motors ensure longer flight times and lower energy consumption.
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.
Next-Generation Magnetic Circuit

Brand-new, highly optimized magnetic circuit matches drive requirements exactly. Providing quicker thrust

response and enhanced dynamic performance under all flight conditions.

Brand New Magnetic Circui
Proven Durability Through
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.

Fixed Wing Motor Water Proof Test
Water Ingress Testing
Motor High Temperature Operation Test
High Temperature Operation Test
Motor Low Temperature Operation Testt
Low Temperature Operation Test
Recommended Combinations
Moto
C6225-200KV
Propeller
20×10 / 21×10
ESC
XRotor Pro H130A 14S BLDC IPC
Battery
12S LiPo
Takeoff weight of single motor
20~25kg
Fixed Wing Drone
C6225 CAD
Product NameC6225-200KV
Specification
  • Model
  • Protection level
  • Motor Size
  • Slot& Pole
  • Stator Size
  • Dynamic balance
  • Stator process
  • Bearing
  • Enamelled wire
  • Motor axle diameter
  • Magnet
  • Props mounting dimensions
  • Isolation test
  • Motor mounting dimensions
  • Rated power input
  • Rated power output
  • C6225-200KV
  • IPX5
  • Φ69*H50.9mm
  • 24N28P
  • 62x25mm
  • ≤15mg
  • High standard silicon steel sheet, rust proof, 180℃ high temperature resistance paint-coat
  • Water proof bearing
  • 220℃
  • Φ10mm
  • 160℃
  • 4*M3@D20mm&4*M4@D23mm
  • 500V AC high voltage resistance test
  • 4*M4@D36mm
  • 710W
  • 580W
Specification
  • 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)
  • 200KV
  • LiPo-12S (48V)
  • 3.4A
  • 86A
  • 4.5kg(48V@21×10)
  • 14.8kg(48V@21×10)
  • 23.5mΩ
  • enameled wire direct lead-out
  • 100mm
  • 130mm
  • 530g
Recommended application combinations
  • Motor
  • Propeller
  • ESC
  • Battery
  • Takeoff weight of Single motor
  • C6225-200KV
  • 20×10/21×10
  • XRotor Pro H130A 14S BLDC IPC
  • 12S LiPo
  • 20~25kg
200KV+20x10 Load Performance Parameters
200KV+20x10 Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

40V(12S LiPo)

20x10

35%

1783

5.3

212.9

2914

8.4

0.48

147.5

/

37%

1957 

6.0 

240.2 

3059 

8.1 

0.53 

170.0 

39%

2142 

6.7 

269.7 

3205 

7.9 

0.58 

195.0 

42%

2438 

7.9 

317.6 

3420 

7.7 

0.66 

236.6 

45%

2750 

9.2 

369.9 

3629 

7.4 

0.74 

282.9 

48%

3074 

10.6 

426.4 

3830 

7.2 

0.83 

333.6 

51%

3411 

12.2 

487.7 

4026 

7.0 

0.92 

389.1 

54%

3760 

13.8 

554.3 

4218 

6.8 

1.02 

449.6 

57%

4123 

15.7 

627.2 

4409 

6.6 

1.12 

516.0 

60%

4502 

17.7 

707.4 

4602 

6.4 

1.22 

589.2 

63%

4900 

19.9 

796.1 

4799 

6.2 

1.33 

670.2 

66%

5318 

22.3 

894.5 

5000 

5.9 

1.45 

759.8 

69%

5759 

25.1 

1003.6 

5206 

5.7 

1.58 

858.8 

72%

6222 

28.1 

1123.9 

5415 

5.5 

1.71 

967.3 

75%

6707 

31.3 

1255.6 

5624 

5.3 

1.84 

1084.9 

78%

7210 

34.9 

1397.7 

5829 

5.2 

1.98 

1210.4 

81%

7725 

38.7 

1548.5 

6024 

5.0 

2.13 

1341.3 

84%

8244 

42.6 

1704.6 

6205 

4.8 

2.27 

1475.2 

87%

8756 

46.5 

1861.6 

6369 

4.7 

2.41 

1609.2 

90%

9244 

50.3 

2013.4 

6517 

4.6 

2.55 

1740.9 

100%

10410 

59.4 

2380.1 

6878 

4.4 

2.91 

2092.8 

*The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input, for reference only.
200KV+20x10 Load Performance Parameters
200KV+20x10 Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

44V(12S LiPo)

20x10

35%

2084

6.0

263.6

3158

7.9

0.56

186.2

/

37%

2293 

6.7 

296.4 

3309 

7.7 

0.62 

214.7 

39%

2514 

7.5 

332.4 

3463 

7.6 

0.68 

246.3 

42%

2864 

8.9 

392.1 

3692 

7.3 

0.77 

298.9 

45%

3233 

10.4 

458.6 

3919 

7.1 

0.87 

357.8 

48%

3618 

12.1 

532.0 

4140 

6.8 

0.98 

422.7 

51%

4019 

13.9 

612.7 

4357 

6.6 

1.08 

494.1 

54%

4436 

15.9 

701.5 

4570 

6.3 

1.20 

572.6 

57%

4872 

18.1 

799.2 

4780 

6.1 

1.32 

658.8 

60%

5328 

20.6 

906.7 

4990 

5.9 

1.44 

753.8 

63%

5805 

23.3 

1025.3 

5201 

5.7 

1.58 

858.7 

66%

6306 

26.2 

1155.9 

5414 

5.5 

1.72 

974.5 

69%

6831 

29.5 

1299.4 

5629 

5.3 

1.87 

1102.0 

72%

7378 

33.0 

1456.3 

5847 

5.1 

2.03 

1242.0 

75%

7946 

36.9 

1626.5 

6066 

4.9 

2.19 

1393.9 

78%

8528 

41.0 

1809.3 

6285 

4.7 

2.37 

1557.4 

81%

9118 

45.4 

2002.8 

6500 

4.6 

2.54 

1730.4 

84%

9703 

50.0 

2204.1 

6706 

4.4 

2.72 

1909.5 

87%

10270 

54.6 

2408.2 

6897 

4.3 

2.89 

2089.9 

90%

10800 

59.2 

2607.8 

7068 

4.1 

3.06 

2265.3 

100%

11960 

69.9 

3081.3 

7409 

3.9 

3.45 

2675.8 

*The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input, for reference only.
200KV+20x10 Load Performance Parameters
200KV+20x10 Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

48V(12S LiPo)

20x10

35%

2421

6.8

326.5

3401

7.4

0.66

235.4

85℃

37%

2669 

7.7 

370.2 

3567 

7.2 

0.73 

272.0 

39%

2931 

8.7 

416.8 

3734 

7.0 

0.80 

312.5 

42%

3342 

10.2 

491.9 

3980 

6.8 

0.91 

379.7 

45%

3768 

11.9 

574.1 

4221 

6.6 

1.03 

454.3 

48%

4207 

13.8 

664.1 

4455 

6.3 

1.15 

536.1 

51%

4658 

15.9 

763.2 

4683 

6.1 

1.28 

625.3 

54%

5124 

18.2 

872.7 

4909 

5.9 

1.41 

722.8 

57%

5607 

20.7 

994.1 

5134 

5.6 

1.54 

829.9 

60%

6113 

23.5 

1128.9 

5361 

5.4 

1.69 

948.0 

63%

6646 

26.6 

1278.5 

5591 

5.2 

1.84 

1078.9 

66%

7208 

30.0 

1444.0 

5824 

5.0 

2.01 

1223.8 

69%

7804 

33.8 

1625.8 

6059 

4.8 

2.18 

1383.9 

72%

8431 

37.9 

1823.8 

6293 

4.6 

2.37 

1559.5 

75%

9087 

42.4 

2037.5 

6525 

4.5 

2.56 

1751.1 

78%

9765 

47.2 

2267.1 

6749 

4.3 

2.77 

1956.8 

81%

10452 

52.3 

2513.6 

6965 

4.2 

2.98 

2176.1 

84%

11131 

57.8 

2778.8 

7171 

4.0 

3.21 

2406.7 

87%

11779 

63.7 

3063.0 

7370 

3.8 

3.43 

2646.0 

90%

12366 

69.9 

3358.7 

7562 

3.7 

3.65 

2886.8 

100%

13329 

82.5 

3964.4 

7932 

3.4 

4.05 

3359.9 

*The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input. The motor temperature is measured after running for 10 minutes at 90% throttle, for reference only.
200KV+21x10 Load Performance Parameters
200KV+21x10 Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

40V(12S LiPo)

21x10

35%

1905

5.2

207.7

2894

9.2

0.51

155.2

/

37%

2100 

6.0 

239.2 

3036 

8.8 

0.56 

178.8 

39%

2302 

6.8 

272.6 

3177 

8.4 

0.62 

204.7 

42%

2617 

8.1 

326.3 

3388 

8.0 

0.70 

248.1 

45%

2945 

9.6 

384.2 

3595 

7.7 

0.79 

296.8 

48%

3287 

11.1 

446.5 

3798 

7.4 

0.88 

350.7 

51%

3644 

12.8 

513.7 

3997 

7.1 

0.98 

410.2 

54%

4019 

14.6 

586.6 

4195 

6.9 

1.08 

475.7 

57%

4414 

16.6 

666.0 

4391 

6.6 

1.19 

547.7 

60%

4831 

18.8 

753.0 

4586 

6.4 

1.30 

626.6 

63%

5273 

21.2 

848.6 

4781 

6.2 

1.42 

713.1 

66%

5742 

23.8 

953.9 

4977 

6.0 

1.55 

808.2 

69%

6237 

26.7 

1069.8 

5174 

5.8 

1.68 

912.3 

72%

6756 

29.9 

1197.0 

5373 

5.6 

1.82 

1026.2 

75%

7298 

33.3 

1335.7 

5572 

5.5 

1.97 

1149.9 

78%

7855 

37.1 

1485.1 

5770 

5.3 

2.12 

1283.0 

81%

8419 

41.0 

1643.4 

5966 

5.1 

2.28 

1424.3 

84%

8979 

45.1 

1807.4 

6156 

5.0 

2.44 

1570.5 

87%

9519 

49.2 

1971.8 

6336 

4.8 

2.59 

1716.7 

90%

10020 

53.2 

2129.2 

6498 

4.7 

2.73 

1854.8 

100%

11076 

61.7 

2472.8 

6821 

4.5 

3.00 

2142.7 

*The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input. The motor temperature is measured after running for 10 minutes at 90% throttle, for reference only.
200KV+21x10 Load Performance Parameters
200KV+21x10 Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

44V(12S LiPo)

21x10

35%

2174

6.2

273.2

3124

8.0

0.59

192.6

/

37%

2407 

7.0 

309.9 

3279 

7.8 

0.65 

222.9 

39%

2658 

7.9 

350.3 

3436 

7.6 

0.71 

257.2 

42%

3056 

9.5 

416.9 

3670 

7.3 

0.82 

315.2 

45%

3472 

11.1 

490.0 

3897 

7.1 

0.93 

380.0 

48%

3898 

12.9 

569.4 

4116 

6.8 

1.05 

450.8 

51%

4332 

14.9 

655.3 

4327 

6.6 

1.16 

527.1 

54%

4776 

17.0 

748.2 

4535 

6.4 

1.28 

609.6 

57%

5233 

19.3 

849.4 

4741 

6.2 

1.41 

698.9 

60%

5709 

21.8 

960.3 

4948 

5.9 

1.54 

796.3 

63%

6209 

24.6 

1082.4 

5158 

5.7 

1.67 

903.4 

66%

6738 

27.6 

1217.5 

5373 

5.5 

1.82 

1022.0 

69%

7302 

31.0 

1366.7 

5592 

5.3 

1.97 

1153.5 

72%

7900 

34.7 

1530.8 

5814 

5.2 

2.13 

1299.1 

75%

8533 

38.8 

1709.6 

6033 

5.0 

2.31 

1458.4 

78%

9196 

43.1 

1901.9 

6247 

4.8 

2.49 

1631.1 

81%

9877 

47.8 

2105.7 

6451 

4.7 

2.69 

1814.7 

84%

10561 

52.6 

2318.2 

6642 

4.6 

2.88 

2005.5 

87%

11225 

57.5 

2535.0 

6823 

4.4 

3.08 

2199.1 

90%

11838 

62.4 

2748.7 

6997 

4.3 

3.26 

2388.9 

100%

12940 

72.2 

3183.0 

7372 

4.1 

3.59 

2774.0 

*The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input, for reference only.
200KV+21x10 Load Performance Parameters
200KV+21x10 Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

48V(12S LiPo)

21x10

35%

2625

7.1

339.1

3385

7.7

0.72

253.7

87℃

37%

2876 

7.9 

381.1 

3544 

7.5 

0.79 

291.4 

39%

3139 

8.9 

427.8 

3704 

7.3 

0.86 

332.5 

42%

3554 

10.5 

506.5 

3945 

7.0 

0.97 

400.8 

45%

3995 

12.4 

595.7 

4185 

6.7 

1.09 

477.5 

48%

4465 

14.5 

695.4 

4423 

6.4 

1.22 

563.0 

51%

4963 

16.8 

805.8 

4659 

6.2 

1.35 

658.1 

54%

5492 

19.3 

926.9 

4891 

5.9 

1.49 

763.1 

57%

6052 

22.0 

1059.3 

5120 

5.7 

1.64 

879.0 

60%

6643 

25.0 

1203.4 

5345 

5.5 

1.80 

1006.4 

63%

7264 

28.3 

1360.3 

5568 

5.3 

1.97 

1146.2 

66%

7914 

31.9 

1531.3 

5790 

5.2 

2.14 

1299.5 

69%

8590 

35.7 

1718.1 

6012 

5.0 

2.33 

1467.2 

72%

9288 

40.0 

1922.4 

6236 

4.8 

2.53 

1650.2 

75%

10000 

44.6 

2145.9 

6463 

4.7 

2.73 

1848.9 

78%

10719 

49.7 

2388.9 

6692 

4.5 

2.94 

2063.0 

81%

11435 

55.1 

2650.2 

6919 

4.3 

3.16 

2290.1 

84%

12134 

60.9 

2925.7 

7139 

4.1 

3.38 

2526.1 

87%

12801 

66.7 

3207.5 

7343 

4.0 

3.59 

2763.5 

90%

13417 

72.5 

3484.2 

7520 

3.9 

3.80 

2991.7 

100%

14809 

86.5 

4157.4 

7845 

3.6 

4.29 

3522.8 

*The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input. The motor temperature is measured after running for 10 minutes at 90% throttle, for reference only.
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Manuals & Documents

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FAQ

C6225
Hobbywing C6225 Fixed Wing Motor
C6225
Universally Versatile Propulsion
Perfectly suited for both fixed-wing cruise and vertical take-off and landing (VTOL) drones
Efficient Cooling with Great Power
Drone Propeller Motor
Paired with
21-inch propellers
the motor delivers up to
a maximum thrust of
14.8kg at 48V
easily handling the dynamic thrust
needs during rapid maneuvers and
sudden payload changes
Efficient Heat Dissipation C6225 Fixed Wing Motor 220kv
Optimized rectangular outlet and
centrifugal fan design reduce
resistance and turbulence,
dramatically improving
heat dissipation
The motor dissipation efficiency improves by 20%
The winding temperature rise is
significantly reduced compared
tomotors of other brands with
similar specifications, ensuring
stable and long-term operation
even in high-load flight conditions
High Protection,
Superior Reliability
High Protection Drone Electric Motor
The motor is designed with
upper and
lower steel
mesh structure

Effectively prevents
ingress of particles
1 mm and larger
in diameter.

Adapts to harsh
flight environments
such as dust and rain
Flexible Choice,
Convenient Application
Intelligent Propeller Control Component Of Uav Motor
  • The stator base is compatible with an IPC
  • (Intelligent Propeller Control) component,
  • allowing for flexible selection.
Paired With An Ipc Esc
  • Paired with an IPC ESC, users can customize
  • the propeller stopping position to minimize
  • the risk of colliding with the ground.
Rotor Bracket
  • The rotor bracket adopts a boss clearance design that effectively prevents
  • interference with the propeller root edge structure, ensuring seamless compatibility
  • and secure installation for both non-folding and folding propellers.
Drone Motor With Propeller eVTOL Motor
  • Supports multiple mounting configurations
  • for quick adaptation, to meet the demands of diverse applications.
Superior Material and
Design for a Safer Flight
Anti Loosening Design
Anti-Loosening Design
The rotor shaft end is fixed by copper washers, circlips, and screws to enhance motor reliability.
Triple Bearing Architecture
Triple-Bearing
Architecture
The triple-bearing architecture optimizes dynamic balance, enhancing impact resistance and durability of the motor to ensure safe flights.
Silicon Steel And Enameled Wires
Silicon Steel and
Enameled Wires
t is designed with industry-leading 0.2mm low-loss silicon steel cores and high-grade 220°C temperature-resistant enameled wires.
Magnet Segment
Magnet Segment
High-grade, strong magnetic arc-shaped magnets boost magnetic energy density for superior torque during climbs and heavy lifts. Cruise efficiency gains of 2–4% over comparable motors ensure longer flight times and lower energy consumption.
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.
Next-Generation Magnetic Circuit

Brand-new, highly optimized magnetic circuit matches drive requirements exactly. Providing quicker thrust

response and enhanced dynamic performance under all flight conditions.

Brand New Magnetic Circui
Proven Durability Through
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.

Fixed Wing Motor Water Proof Test
Water Ingress Testing
Motor High Temperature Operation Test
High Temperature Operation Test
Motor Low Temperature Operation Testt
Low Temperature Operation Test
Recommended Combinations
Moto
C6225-200KV
Propeller
20×10 / 21×10
ESC
XRotor Pro H130A 14S BLDC IPC
Battery
12S LiPo
Takeoff weight of single motor
20~25kg
Fixed Wing Drone
C6225 CAD
Product NameC6225-200KV
Specification
  • Model
  • Protection level
  • Motor Size
  • Slot& Pole
  • Stator Size
  • Dynamic balance
  • Stator process
  • Bearing
  • Enamelled wire
  • Motor axle diameter
  • Magnet
  • Props mounting dimensions
  • Isolation test
  • Motor mounting dimensions
  • Rated power input
  • Rated power output
  • C6225-200KV
  • IPX5
  • Φ69*H50.9mm
  • 24N28P
  • 62x25mm
  • ≤15mg
  • High standard silicon steel sheet, rust proof, 180℃ high temperature resistance paint-coat
  • Water proof bearing
  • 220℃
  • Φ10mm
  • 160℃
  • 4*M3@D20mm&4*M4@D23mm
  • 500V AC high voltage resistance test
  • 4*M4@D36mm
  • 710W
  • 580W
Specification
  • 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)
  • 200KV
  • LiPo-12S (48V)
  • 3.4A
  • 86A
  • 4.5kg(48V@21×10)
  • 14.8kg(48V@21×10)
  • 23.5mΩ
  • enameled wire direct lead-out
  • 100mm
  • 130mm
  • 530g
Recommended application combinations
  • Motor
  • Propeller
  • ESC
  • Battery
  • Takeoff weight of Single motor
  • C6225-200KV
  • 20×10/21×10
  • XRotor Pro H130A 14S BLDC IPC
  • 12S LiPo
  • 20~25kg
200KV+20x10 Load Performance Parameters
200KV+20x10 Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

40V(12S LiPo)

20x10

35%

1783

5.3

212.9

2914

8.4

0.48

147.5

/

37%

1957 

6.0 

240.2 

3059 

8.1 

0.53 

170.0 

39%

2142 

6.7 

269.7 

3205 

7.9 

0.58 

195.0 

42%

2438 

7.9 

317.6 

3420 

7.7 

0.66 

236.6 

45%

2750 

9.2 

369.9 

3629 

7.4 

0.74 

282.9 

48%

3074 

10.6 

426.4 

3830 

7.2 

0.83 

333.6 

51%

3411 

12.2 

487.7 

4026 

7.0 

0.92 

389.1 

54%

3760 

13.8 

554.3 

4218 

6.8 

1.02 

449.6 

57%

4123 

15.7 

627.2 

4409 

6.6 

1.12 

516.0 

60%

4502 

17.7 

707.4 

4602 

6.4 

1.22 

589.2 

63%

4900 

19.9 

796.1 

4799 

6.2 

1.33 

670.2 

66%

5318 

22.3 

894.5 

5000 

5.9 

1.45 

759.8 

69%

5759 

25.1 

1003.6 

5206 

5.7 

1.58 

858.8 

72%

6222 

28.1 

1123.9 

5415 

5.5 

1.71 

967.3 

75%

6707 

31.3 

1255.6 

5624 

5.3 

1.84 

1084.9 

78%

7210 

34.9 

1397.7 

5829 

5.2 

1.98 

1210.4 

81%

7725 

38.7 

1548.5 

6024 

5.0 

2.13 

1341.3 

84%

8244 

42.6 

1704.6 

6205 

4.8 

2.27 

1475.2 

87%

8756 

46.5 

1861.6 

6369 

4.7 

2.41 

1609.2 

90%

9244 

50.3 

2013.4 

6517 

4.6 

2.55 

1740.9 

100%

10410 

59.4 

2380.1 

6878 

4.4 

2.91 

2092.8 

*The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input, for reference only.
200KV+20x10 Load Performance Parameters
200KV+20x10 Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

44V(12S LiPo)

20x10

35%

2084

6.0

263.6

3158

7.9

0.56

186.2

/

37%

2293 

6.7 

296.4 

3309 

7.7 

0.62 

214.7 

39%

2514 

7.5 

332.4 

3463 

7.6 

0.68 

246.3 

42%

2864 

8.9 

392.1 

3692 

7.3 

0.77 

298.9 

45%

3233 

10.4 

458.6 

3919 

7.1 

0.87 

357.8 

48%

3618 

12.1 

532.0 

4140 

6.8 

0.98 

422.7 

51%

4019 

13.9 

612.7 

4357 

6.6 

1.08 

494.1 

54%

4436 

15.9 

701.5 

4570 

6.3 

1.20 

572.6 

57%

4872 

18.1 

799.2 

4780 

6.1 

1.32 

658.8 

60%

5328 

20.6 

906.7 

4990 

5.9 

1.44 

753.8 

63%

5805 

23.3 

1025.3 

5201 

5.7 

1.58 

858.7 

66%

6306 

26.2 

1155.9 

5414 

5.5 

1.72 

974.5 

69%

6831 

29.5 

1299.4 

5629 

5.3 

1.87 

1102.0 

72%

7378 

33.0 

1456.3 

5847 

5.1 

2.03 

1242.0 

75%

7946 

36.9 

1626.5 

6066 

4.9 

2.19 

1393.9 

78%

8528 

41.0 

1809.3 

6285 

4.7 

2.37 

1557.4 

81%

9118 

45.4 

2002.8 

6500 

4.6 

2.54 

1730.4 

84%

9703 

50.0 

2204.1 

6706 

4.4 

2.72 

1909.5 

87%

10270 

54.6 

2408.2 

6897 

4.3 

2.89 

2089.9 

90%

10800 

59.2 

2607.8 

7068 

4.1 

3.06 

2265.3 

100%

11960 

69.9 

3081.3 

7409 

3.9 

3.45 

2675.8 

*The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input, for reference only.
200KV+20x10 Load Performance Parameters
200KV+20x10 Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

48V(12S LiPo)

20x10

35%

2421

6.8

326.5

3401

7.4

0.66

235.4

85℃

37%

2669 

7.7 

370.2 

3567 

7.2 

0.73 

272.0 

39%

2931 

8.7 

416.8 

3734 

7.0 

0.80 

312.5 

42%

3342 

10.2 

491.9 

3980 

6.8 

0.91 

379.7 

45%

3768 

11.9 

574.1 

4221 

6.6 

1.03 

454.3 

48%

4207 

13.8 

664.1 

4455 

6.3 

1.15 

536.1 

51%

4658 

15.9 

763.2 

4683 

6.1 

1.28 

625.3 

54%

5124 

18.2 

872.7 

4909 

5.9 

1.41 

722.8 

57%

5607 

20.7 

994.1 

5134 

5.6 

1.54 

829.9 

60%

6113 

23.5 

1128.9 

5361 

5.4 

1.69 

948.0 

63%

6646 

26.6 

1278.5 

5591 

5.2 

1.84 

1078.9 

66%

7208 

30.0 

1444.0 

5824 

5.0 

2.01 

1223.8 

69%

7804 

33.8 

1625.8 

6059 

4.8 

2.18 

1383.9 

72%

8431 

37.9 

1823.8 

6293 

4.6 

2.37 

1559.5 

75%

9087 

42.4 

2037.5 

6525 

4.5 

2.56 

1751.1 

78%

9765 

47.2 

2267.1 

6749 

4.3 

2.77 

1956.8 

81%

10452 

52.3 

2513.6 

6965 

4.2 

2.98 

2176.1 

84%

11131 

57.8 

2778.8 

7171 

4.0 

3.21 

2406.7 

87%

11779 

63.7 

3063.0 

7370 

3.8 

3.43 

2646.0 

90%

12366 

69.9 

3358.7 

7562 

3.7 

3.65 

2886.8 

100%

13329 

82.5 

3964.4 

7932 

3.4 

4.05 

3359.9 

*The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input. The motor temperature is measured after running for 10 minutes at 90% throttle, for reference only.
200KV+21x10 Load Performance Parameters
200KV+21x10 Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

40V(12S LiPo)

21x10

35%

1905

5.2

207.7

2894

9.2

0.51

155.2

/

37%

2100 

6.0 

239.2 

3036 

8.8 

0.56 

178.8 

39%

2302 

6.8 

272.6 

3177 

8.4 

0.62 

204.7 

42%

2617 

8.1 

326.3 

3388 

8.0 

0.70 

248.1 

45%

2945 

9.6 

384.2 

3595 

7.7 

0.79 

296.8 

48%

3287 

11.1 

446.5 

3798 

7.4 

0.88 

350.7 

51%

3644 

12.8 

513.7 

3997 

7.1 

0.98 

410.2 

54%

4019 

14.6 

586.6 

4195 

6.9 

1.08 

475.7 

57%

4414 

16.6 

666.0 

4391 

6.6 

1.19 

547.7 

60%

4831 

18.8 

753.0 

4586 

6.4 

1.30 

626.6 

63%

5273 

21.2 

848.6 

4781 

6.2 

1.42 

713.1 

66%

5742 

23.8 

953.9 

4977 

6.0 

1.55 

808.2 

69%

6237 

26.7 

1069.8 

5174 

5.8 

1.68 

912.3 

72%

6756 

29.9 

1197.0 

5373 

5.6 

1.82 

1026.2 

75%

7298 

33.3 

1335.7 

5572 

5.5 

1.97 

1149.9 

78%

7855 

37.1 

1485.1 

5770 

5.3 

2.12 

1283.0 

81%

8419 

41.0 

1643.4 

5966 

5.1 

2.28 

1424.3 

84%

8979 

45.1 

1807.4 

6156 

5.0 

2.44 

1570.5 

87%

9519 

49.2 

1971.8 

6336 

4.8 

2.59 

1716.7 

90%

10020 

53.2 

2129.2 

6498 

4.7 

2.73 

1854.8 

100%

11076 

61.7 

2472.8 

6821 

4.5 

3.00 

2142.7 

*The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input. The motor temperature is measured after running for 10 minutes at 90% throttle, for reference only.
200KV+21x10 Load Performance Parameters
200KV+21x10 Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

44V(12S LiPo)

21x10

35%

2174

6.2

273.2

3124

8.0

0.59

192.6

/

37%

2407 

7.0 

309.9 

3279 

7.8 

0.65 

222.9 

39%

2658 

7.9 

350.3 

3436 

7.6 

0.71 

257.2 

42%

3056 

9.5 

416.9 

3670 

7.3 

0.82 

315.2 

45%

3472 

11.1 

490.0 

3897 

7.1 

0.93 

380.0 

48%

3898 

12.9 

569.4 

4116 

6.8 

1.05 

450.8 

51%

4332 

14.9 

655.3 

4327 

6.6 

1.16 

527.1 

54%

4776 

17.0 

748.2 

4535 

6.4 

1.28 

609.6 

57%

5233 

19.3 

849.4 

4741 

6.2 

1.41 

698.9 

60%

5709 

21.8 

960.3 

4948 

5.9 

1.54 

796.3 

63%

6209 

24.6 

1082.4 

5158 

5.7 

1.67 

903.4 

66%

6738 

27.6 

1217.5 

5373 

5.5 

1.82 

1022.0 

69%

7302 

31.0 

1366.7 

5592 

5.3 

1.97 

1153.5 

72%

7900 

34.7 

1530.8 

5814 

5.2 

2.13 

1299.1 

75%

8533 

38.8 

1709.6 

6033 

5.0 

2.31 

1458.4 

78%

9196 

43.1 

1901.9 

6247 

4.8 

2.49 

1631.1 

81%

9877 

47.8 

2105.7 

6451 

4.7 

2.69 

1814.7 

84%

10561 

52.6 

2318.2 

6642 

4.6 

2.88 

2005.5 

87%

11225 

57.5 

2535.0 

6823 

4.4 

3.08 

2199.1 

90%

11838 

62.4 

2748.7 

6997 

4.3 

3.26 

2388.9 

100%

12940 

72.2 

3183.0 

7372 

4.1 

3.59 

2774.0 

*The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input, for reference only.
200KV+21x10 Load Performance Parameters
200KV+21x10 Motor Propeller Pull Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power Input(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Motor Temperature(℃)

48V(12S LiPo)

21x10

35%

2625

7.1

339.1

3385

7.7

0.72

253.7

87℃

37%

2876 

7.9 

381.1 

3544 

7.5 

0.79 

291.4 

39%

3139 

8.9 

427.8 

3704 

7.3 

0.86 

332.5 

42%

3554 

10.5 

506.5 

3945 

7.0 

0.97 

400.8 

45%

3995 

12.4 

595.7 

4185 

6.7 

1.09 

477.5 

48%

4465 

14.5 

695.4 

4423 

6.4 

1.22 

563.0 

51%

4963 

16.8 

805.8 

4659 

6.2 

1.35 

658.1 

54%

5492 

19.3 

926.9 

4891 

5.9 

1.49 

763.1 

57%

6052 

22.0 

1059.3 

5120 

5.7 

1.64 

879.0 

60%

6643 

25.0 

1203.4 

5345 

5.5 

1.80 

1006.4 

63%

7264 

28.3 

1360.3 

5568 

5.3 

1.97 

1146.2 

66%

7914 

31.9 

1531.3 

5790 

5.2 

2.14 

1299.5 

69%

8590 

35.7 

1718.1 

6012 

5.0 

2.33 

1467.2 

72%

9288 

40.0 

1922.4 

6236 

4.8 

2.53 

1650.2 

75%

10000 

44.6 

2145.9 

6463 

4.7 

2.73 

1848.9 

78%

10719 

49.7 

2388.9 

6692 

4.5 

2.94 

2063.0 

81%

11435 

55.1 

2650.2 

6919 

4.3 

3.16 

2290.1 

84%

12134 

60.9 

2925.7 

7139 

4.1 

3.38 

2526.1 

87%

12801 

66.7 

3207.5 

7343 

4.0 

3.59 

2763.5 

90%

13417 

72.5 

3484.2 

7520 

3.9 

3.80 

2991.7 

100%

14809 

86.5 

4157.4 

7845 

3.6 

4.29 

3522.8 

*The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input. The motor temperature is measured after running for 10 minutes at 90% throttle, for reference only.
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