M6210 HighProt - 170/320KV Multirotor Drone Motors 12/6S
M6210 HighProt
Specially designed for multi-rotor drones.
High efficiency, strong protection, and high reliability.
M6210 HighProt
11kg
They are suitable for UAVs (quadrotor)
with a take-off weight of 11kg.
M6210 HighProt motor uses two different core stack thicknesses in order to meet different
payload application requirements.
An Abundance of Drone Applications
Brand-new Magnetic Circuit Design
Optimises the electromotive force harmonics. It creates a sinusoidal motion to perfectly matched with the ESC.
High Quality Materials and
Strong Protective Capabilities
The bracket and bottom cover of the motor are designed with a semi-enclosed structure with dust-proof grilles.
Regardless of how the motor is being installed,it can effectively resist dust and sand.
Excellent nickel-plating 
electrophoresis
treatment process
for the casing.
High toughness
carbide main shaft.
The back cover and the stator
base are designed separately,
and the outlet position is protected
by a rubber wire buckle to facilitate
waterproofing with the holes
in the motor base.
High-performance
iron core made from
low-loss silicon
steel sheets from
top-tier brands.
Silicon steel sheets
adopt new anti-rust and
anti-corrosion
treatment technology.
The motor is certified by NSS48.
The motor adopts a motor shaft end cir-clip + pressure ring + screw interlocking
structure to ensure safety and to prevent it from falling off.
Recommended Combinations
  • Motor
    M6210 HighProt-170KV
    M6210 HighProt-320KV
     

    Battery
    12S LiPo
    6S LiPo
  • Propeller
    MSC 21x6.3
    MSC 22x7.8
    MPF 22x7.0

    Thrust/rotor
    2.2~2.7kg
  • ESC
    XRotor Pro H60A 14S
    XRotor Pro H60A 6S
     

    Takeoff weight of quadrotor
    9.0~11.0kg

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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By submitting this form, you agree to HOBBYWING's Privacy Policy
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M6210 HighProt CAD
Model
M6210 HighProt
Specification
KV 170 320
Motor Size Φ68.7*H30.2mm Φ68.7*H30.2mm
Stator process High standard silicon steel sheet, rust proof, 180℃ high temperature resistance paint-coat High standard silicon steel sheet, rust proof, 180℃ high temperature resistance paint-coat
Enamelled wire 200℃ 200℃
Magnet 150℃ 150℃
Isolation test 500V AC high voltage resistance test 500V AC high voltage resistance test
Protection level IP45 IP45
Slot& Pole 24N28P 24N28P
Dynamic balance ≤8mg ≤8mg
Bearing Water proof bearing Water proof bearing
Motor axle diameter Φ6mm Φ6mm
Props mounting dimensions 4×M3@D12mm,4×M3@D18mm 4×M3@D12mm,4×M3@D18mm
Motor mounting dimensions 4×M4@D25mm 4×M4@D25mm
Rated output power (Max continuous) 306W 306W
Specification
Battery(LiPo) 12S LiPo 6S LiPo
No-load current 1.31A 1.97A
Maximum current (Non-hermeticAmbient Temperature ≤ 25℃) 42.9A 55.2A
Max thrust 9.1kg 7.1kg
Resistance 98.6mΩ 33.65mΩ
Wire Size 16AWG 16AWG
Wire length 150mm 150mm
Weight(With wire) 231g 239g
Recommended application combinations
Propeller MSC 21x6.3 / MSC 22x7.8 / MFP 22x7.0 MSC 21x6.3 / MSC 22x7.8 / MFP 22x7.0
ESC XRotor Pro H60A 14S XRotor Pro H60A 6S
Battery 12S LiPo 6S LiPo
Thrust/rotor 2.2~2.7kg 2.2~2.7kg
Takeoff weight of quadrotor 9.0~11.0kg 9.0~11.0kg
M6210 170KV+MSC 21x6.3 Load Performance Parameters
M6210 170KV+MSC 21x6.3 Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Temperature(℃)

46V (12S LiPo)

MSC 21x6.3

33%

1104

2.0

92.3

2572

12.0

0.26

69.6

46.7

35%

1235 

2.3 

106.6 

2721 

11.6 

0.29 

82.2 

37%

1381 

2.7 

123.4 

2877 

11.2 

0.32 

97.0 

39%

1537 

3.1 

142.2 

3035 

10.8 

0.36 

113.7 

42%

1786 

3.8 

173.9 

3268 

10.3 

0.42 

142.0 

45%

2044 

4.5 

208.9 

3489 

9.8 

0.47 

173.3 

48%

2307 

5.4 

246.8 

3698 

9.3 

0.53 

207.1 

51%

2572 

6.2 

287.1 

3896 

9.0 

0.60 

242.9 

54%

2840 

7.2 

330.0 

4084 

8.6 

0.66 

280.8 

57%

3111 

8.2 

375.6 

4267 

8.3 

0.72 

321.1 

60%

3389 

9.2 

424.3 

4446 

8.0 

0.78 

364.1 

63%

3677 

10.4 

477.0 

4625 

7.7 

0.85 

410.5 

66%

3977 

11.6 

534.3 

4806 

7.4 

0.92 

461.0 

69%

4293 

13.0 

597.0 

4989 

7.2 

0.99 

516.3 

72%

4625 

14.5 

665.8 

5176 

6.9 

1.06 

576.9 

75%

4974 

16.1 

740.9 

5364 

6.7 

1.14 

642.9 

78%

5337 

17.9 

822.3 

5550 

6.5 

1.23 

714.2 

81%

5709 

19.8 

909.3 

5733 

6.3 

1.32 

789.5 

84%

6082 

21.7 

1000.0 

5906 

6.1 

1.40 

867.3 

87%

6444 

23.7 

1091.6 

6069 

5.9 

1.49 

944.7 

90%

6778 

25.6 

1179.5 

6215 

5.7 

1.56 

1018.1 

100%

7383 

29.3 

1346.5 

6487 

5.5 

1.70 

1156.1 

*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 65% throttle, for reference only.
M6210 170KV+MSC 22x7.8 Load Performance Parameters
M6210 170KV+MSC 22x7.8 Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Temperature(℃)

46V (12S LiPo)

MSC 22x7.8

33%

1525

3.0

136.5

2513

11.2

0.42

110.4

55.6

35%

1719 

3.4 

158.5 

2659 

10.8 

0.47 

130.4 

37%

1920 

4.0 

184.0 

2806 

10.4 

0.52 

152.8 

39%

2128 

4.6 

212.5 

2952 

10.0 

0.57 

177.4 

42%

2447 

5.7 

260.3 

3165 

9.4 

0.66 

218.1 

45%

2770 

6.8 

312.7 

3369 

8.9 

0.74 

262.4 

48%

3097 

8.0 

368.9 

3563 

8.4 

0.83 

309.9 

51%

3425 

9.3 

428.3 

3747 

8.0 

0.92 

360.1 

54%

3757 

10.7 

490.9 

3922 

7.7 

1.01 

413.1 

57%

4094 

12.1 

557.1 

4090 

7.3 

1.09 

468.9 

60%

4439 

13.6 

627.8 

4253 

7.1 

1.19 

527.9 

63%

4795 

15.3 

703.9 

4413 

6.8 

1.28 

590.8 

66%

5164 

17.1 

786.8 

4572 

6.6 

1.37 

658.2 

69%

5548 

19.1 

877.6 

4731 

6.3 

1.47 

730.6 

72%

5948 

21.2 

977.7 

4891 

6.1 

1.58 

808.7 

75%

6361 

23.6 

1087.7 

5052 

5.8 

1.69 

892.6 

78%

6784 

26.2 

1207.8 

5212 

5.6 

1.80 

982.2 

81%

7213 

29.0 

1336.7 

5369 

5.4 

1.91 

1076.4 

84%

7637 

31.9 

1471.0 

5519 

5.2 

2.03 

1172.9 

87%

8045 

34.9 

1605.3 

5656 

5.0 

2.14 

1268.1 

90%

8421 

37.6 

1732.0 

5774 

4.9 

2.24 

1356.7 

100%

9137 

42.9 

1973.1 

5962 

4.6 

2.44 

1522.7 

*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 65% throttle, for reference only.
M6210 320KV+MSC 21x6.3 Load Performance Parameters
M6210 320KV+MSC 21x6.3 Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Temperature(℃)

23V (6S LiPo)

MSC 21x6.3

33%

842

2.9

66.5

2234

12.7

0.21

49.0

49.1

35%

944 

3.3 

75.9 

2356 

12.4 

0.23 

57.5 

37%

1056 

3.8 

86.9 

2486 

12.1 

0.26 

67.4 

39%

1174 

4.3 

99.4 

2618 

11.8 

0.29 

78.6 

42%

1363 

5.2 

120.8 

2817 

11.3 

0.33 

97.7 

45%

1560 

6.3 

144.9 

3012 

10.8 

0.38 

119.0 

48%

1764 

7.4 

171.2 

3199 

10.3 

0.42 

142.3 

51%

1971 

8.6 

199.5 

3377 

9.9 

0.47 

167.4 

54%

2182 

10.0 

229.7 

3548 

9.5 

0.52 

194.2 

57%

2398 

11.4 

261.8 

3711 

9.2 

0.57 

222.6 

60%

2618 

12.8 

296.0 

3869 

8.8 

0.62 

252.8 

63%

2844 

14.4 

332.5 

4024 

8.6 

0.68 

285.1 

66%

3077 

16.1 

371.8 

4177 

8.3 

0.73 

319.7 

69%

3318 

18.0 

414.1 

4331 

8.0 

0.79 

357.0 

72%

3568 

19.9 

459.9 

4486 

7.8 

0.85 

397.3 

75%

3826 

22.1 

509.3 

4643 

7.5 

0.91 

440.8 

78%

4091 

24.4 

562.4 

4803 

7.3 

0.97 

487.5 

81%

4360 

26.8 

618.8 

4964 

7.0 

1.03 

537.0 

84%

4629 

29.4 

677.5 

5121 

6.8 

1.10 

588.5 

87%

4893 

32.0 

736.9 

5270 

6.6 

1.16 

640.2 

90%

5143 

34.5 

794.6 

5404 

6.5 

1.22 

690.0 

100%

5717 

40.3 

928.7 

5662 

6.2 

1.35 

800.7 

*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 65% throttle, for reference only.
M6210 320KV+MSC 22x7.8 Load Performance Parameters
M6210 320KV+MSC 22x7.8 Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Temperature(℃)

23V (6S LiPo)

MSC 22x7.8

33%

1094

3.7

86.1

2142

12.7

0.30

66.7

62.0

35%

1218 

4.3 

98.3 

2253 

12.4 

0.33 

77.6 

37%

1359 

4.9 

113.2 

2373 

12.0 

0.36 

90.6 

39%

1512 

5.7 

130.5 

2498 

11.6 

0.40 

105.7 

42%

1757 

7.0 

160.6 

2687 

10.9 

0.47 

131.9 

45%

2015 

8.4 

194.8 

2874 

10.3 

0.54 

161.5 

48%

2280 

10.1 

232.3 

3053 

9.8 

0.61 

193.8 

51%

2549 

11.8 

272.5 

3223 

9.4 

0.68 

228.3 

54%

2819 

13.7 

315.0 

3384 

9.0 

0.75 

264.7 

57%

3091 

15.6 

359.7 

3538 

8.6 

0.82 

302.7 

60%

3367 

17.7 

407.0 

3687 

8.3 

0.89 

342.6 

63%

3646 

19.8 

457.0 

3831 

8.0 

0.96 

384.6 

66%

3932 

22.2 

510.6 

3973 

7.7 

1.03 

429.1 

69%

4226 

24.7 

568.1 

4115 

7.4 

1.11 

476.8 

72%

4530 

27.4 

630.4 

4256 

7.2 

1.18 

528.0 

75%

4843 

30.3 

697.8 

4397 

6.9 

1.27 

583.1 

78%

5165 

33.4 

770.4 

4538 

6.7 

1.35 

642.4 

81%

5492 

36.8 

847.9 

4677 

6.5 

1.44 

705.2 

84%

5821 

40.3 

928.9 

4811 

6.3 

1.53 

770.6 

87%

6143 

43.9 

1011.1 

4935 

6.1 

1.62 

836.4 

90%

6448 

47.4 

1090.9 

5047 

5.9 

1.70 

899.4 

100%

7124 

55.2 

1270.0 

5261 

5.6 

1.88 

1035.0 

*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 65% throttle, for reference only.
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FAQ

M6210 HighProt

 

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.
captcha
By submitting this form, you agree to HOBBYWING's Privacy Policy
Thanks for reaching out!We have received your message and will get back to you shortly.
Best Regards,
HOBBYWING Team
M6210 HighProt CAD
Model
M6210 HighProt
Specification
KV 170 320
Motor Size Φ68.7*H30.2mm Φ68.7*H30.2mm
Stator process High standard silicon steel sheet, rust proof, 180℃ high temperature resistance paint-coat High standard silicon steel sheet, rust proof, 180℃ high temperature resistance paint-coat
Enamelled wire 200℃ 200℃
Magnet 150℃ 150℃
Isolation test 500V AC high voltage resistance test 500V AC high voltage resistance test
Protection level IP45 IP45
Slot& Pole 24N28P 24N28P
Dynamic balance ≤8mg ≤8mg
Bearing Water proof bearing Water proof bearing
Motor axle diameter Φ6mm Φ6mm
Props mounting dimensions 4×M3@D12mm,4×M3@D18mm 4×M3@D12mm,4×M3@D18mm
Motor mounting dimensions 4×M4@D25mm 4×M4@D25mm
Rated output power (Max continuous) 306W 306W
Specification
Battery(LiPo) 12S LiPo 6S LiPo
No-load current 1.31A 1.97A
Maximum current (Non-hermeticAmbient Temperature ≤ 25℃) 42.9A 55.2A
Max thrust 9.1kg 7.1kg
Resistance 98.6mΩ 33.65mΩ
Wire Size 16AWG 16AWG
Wire length 150mm 150mm
Weight(With wire) 231g 239g
Recommended application combinations
Propeller MSC 21x6.3 / MSC 22x7.8 / MFP 22x7.0 MSC 21x6.3 / MSC 22x7.8 / MFP 22x7.0
ESC XRotor Pro H60A 14S XRotor Pro H60A 6S
Battery 12S LiPo 6S LiPo
Thrust/rotor 2.2~2.7kg 2.2~2.7kg
Takeoff weight of quadrotor 9.0~11.0kg 9.0~11.0kg
M6210 170KV+MSC 21x6.3 Load Performance Parameters
M6210 170KV+MSC 21x6.3 Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Temperature(℃)

46V (12S LiPo)

MSC 21x6.3

33%

1104

2.0

92.3

2572

12.0

0.26

69.6

46.7

35%

1235 

2.3 

106.6 

2721 

11.6 

0.29 

82.2 

37%

1381 

2.7 

123.4 

2877 

11.2 

0.32 

97.0 

39%

1537 

3.1 

142.2 

3035 

10.8 

0.36 

113.7 

42%

1786 

3.8 

173.9 

3268 

10.3 

0.42 

142.0 

45%

2044 

4.5 

208.9 

3489 

9.8 

0.47 

173.3 

48%

2307 

5.4 

246.8 

3698 

9.3 

0.53 

207.1 

51%

2572 

6.2 

287.1 

3896 

9.0 

0.60 

242.9 

54%

2840 

7.2 

330.0 

4084 

8.6 

0.66 

280.8 

57%

3111 

8.2 

375.6 

4267 

8.3 

0.72 

321.1 

60%

3389 

9.2 

424.3 

4446 

8.0 

0.78 

364.1 

63%

3677 

10.4 

477.0 

4625 

7.7 

0.85 

410.5 

66%

3977 

11.6 

534.3 

4806 

7.4 

0.92 

461.0 

69%

4293 

13.0 

597.0 

4989 

7.2 

0.99 

516.3 

72%

4625 

14.5 

665.8 

5176 

6.9 

1.06 

576.9 

75%

4974 

16.1 

740.9 

5364 

6.7 

1.14 

642.9 

78%

5337 

17.9 

822.3 

5550 

6.5 

1.23 

714.2 

81%

5709 

19.8 

909.3 

5733 

6.3 

1.32 

789.5 

84%

6082 

21.7 

1000.0 

5906 

6.1 

1.40 

867.3 

87%

6444 

23.7 

1091.6 

6069 

5.9 

1.49 

944.7 

90%

6778 

25.6 

1179.5 

6215 

5.7 

1.56 

1018.1 

100%

7383 

29.3 

1346.5 

6487 

5.5 

1.70 

1156.1 

*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 65% throttle, for reference only.
M6210 170KV+MSC 22x7.8 Load Performance Parameters
M6210 170KV+MSC 22x7.8 Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Temperature(℃)

46V (12S LiPo)

MSC 22x7.8

33%

1525

3.0

136.5

2513

11.2

0.42

110.4

55.6

35%

1719 

3.4 

158.5 

2659 

10.8 

0.47 

130.4 

37%

1920 

4.0 

184.0 

2806 

10.4 

0.52 

152.8 

39%

2128 

4.6 

212.5 

2952 

10.0 

0.57 

177.4 

42%

2447 

5.7 

260.3 

3165 

9.4 

0.66 

218.1 

45%

2770 

6.8 

312.7 

3369 

8.9 

0.74 

262.4 

48%

3097 

8.0 

368.9 

3563 

8.4 

0.83 

309.9 

51%

3425 

9.3 

428.3 

3747 

8.0 

0.92 

360.1 

54%

3757 

10.7 

490.9 

3922 

7.7 

1.01 

413.1 

57%

4094 

12.1 

557.1 

4090 

7.3 

1.09 

468.9 

60%

4439 

13.6 

627.8 

4253 

7.1 

1.19 

527.9 

63%

4795 

15.3 

703.9 

4413 

6.8 

1.28 

590.8 

66%

5164 

17.1 

786.8 

4572 

6.6 

1.37 

658.2 

69%

5548 

19.1 

877.6 

4731 

6.3 

1.47 

730.6 

72%

5948 

21.2 

977.7 

4891 

6.1 

1.58 

808.7 

75%

6361 

23.6 

1087.7 

5052 

5.8 

1.69 

892.6 

78%

6784 

26.2 

1207.8 

5212 

5.6 

1.80 

982.2 

81%

7213 

29.0 

1336.7 

5369 

5.4 

1.91 

1076.4 

84%

7637 

31.9 

1471.0 

5519 

5.2 

2.03 

1172.9 

87%

8045 

34.9 

1605.3 

5656 

5.0 

2.14 

1268.1 

90%

8421 

37.6 

1732.0 

5774 

4.9 

2.24 

1356.7 

100%

9137 

42.9 

1973.1 

5962 

4.6 

2.44 

1522.7 

*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 65% throttle, for reference only.
M6210 320KV+MSC 21x6.3 Load Performance Parameters
M6210 320KV+MSC 21x6.3 Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Temperature(℃)

23V (6S LiPo)

MSC 21x6.3

33%

842

2.9

66.5

2234

12.7

0.21

49.0

49.1

35%

944 

3.3 

75.9 

2356 

12.4 

0.23 

57.5 

37%

1056 

3.8 

86.9 

2486 

12.1 

0.26 

67.4 

39%

1174 

4.3 

99.4 

2618 

11.8 

0.29 

78.6 

42%

1363 

5.2 

120.8 

2817 

11.3 

0.33 

97.7 

45%

1560 

6.3 

144.9 

3012 

10.8 

0.38 

119.0 

48%

1764 

7.4 

171.2 

3199 

10.3 

0.42 

142.3 

51%

1971 

8.6 

199.5 

3377 

9.9 

0.47 

167.4 

54%

2182 

10.0 

229.7 

3548 

9.5 

0.52 

194.2 

57%

2398 

11.4 

261.8 

3711 

9.2 

0.57 

222.6 

60%

2618 

12.8 

296.0 

3869 

8.8 

0.62 

252.8 

63%

2844 

14.4 

332.5 

4024 

8.6 

0.68 

285.1 

66%

3077 

16.1 

371.8 

4177 

8.3 

0.73 

319.7 

69%

3318 

18.0 

414.1 

4331 

8.0 

0.79 

357.0 

72%

3568 

19.9 

459.9 

4486 

7.8 

0.85 

397.3 

75%

3826 

22.1 

509.3 

4643 

7.5 

0.91 

440.8 

78%

4091 

24.4 

562.4 

4803 

7.3 

0.97 

487.5 

81%

4360 

26.8 

618.8 

4964 

7.0 

1.03 

537.0 

84%

4629 

29.4 

677.5 

5121 

6.8 

1.10 

588.5 

87%

4893 

32.0 

736.9 

5270 

6.6 

1.16 

640.2 

90%

5143 

34.5 

794.6 

5404 

6.5 

1.22 

690.0 

100%

5717 

40.3 

928.7 

5662 

6.2 

1.35 

800.7 

*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 65% throttle, for reference only.
M6210 320KV+MSC 22x7.8 Load Performance Parameters
M6210 320KV+MSC 22x7.8 Thrust Test Data

Voltage(V)

Propeller

Throttle(%)

Thrust(g)

Current(A)

Power(W)

Speed(RPM)

Efficiency(g/W)

Torque(N·m)

Power Output(W)

Temperature(℃)

23V (6S LiPo)

MSC 22x7.8

33%

1094

3.7

86.1

2142

12.7

0.30

66.7

62.0

35%

1218 

4.3 

98.3 

2253 

12.4 

0.33 

77.6 

37%

1359 

4.9 

113.2 

2373 

12.0 

0.36 

90.6 

39%

1512 

5.7 

130.5 

2498 

11.6 

0.40 

105.7 

42%

1757 

7.0 

160.6 

2687 

10.9 

0.47 

131.9 

45%

2015 

8.4 

194.8 

2874 

10.3 

0.54 

161.5 

48%

2280 

10.1 

232.3 

3053 

9.8 

0.61 

193.8 

51%

2549 

11.8 

272.5 

3223 

9.4 

0.68 

228.3 

54%

2819 

13.7 

315.0 

3384 

9.0 

0.75 

264.7 

57%

3091 

15.6 

359.7 

3538 

8.6 

0.82 

302.7 

60%

3367 

17.7 

407.0 

3687 

8.3 

0.89 

342.6 

63%

3646 

19.8 

457.0 

3831 

8.0 

0.96 

384.6 

66%

3932 

22.2 

510.6 

3973 

7.7 

1.03 

429.1 

69%

4226 

24.7 

568.1 

4115 

7.4 

1.11 

476.8 

72%

4530 

27.4 

630.4 

4256 

7.2 

1.18 

528.0 

75%

4843 

30.3 

697.8 

4397 

6.9 

1.27 

583.1 

78%

5165 

33.4 

770.4 

4538 

6.7 

1.35 

642.4 

81%

5492 

36.8 

847.9 

4677 

6.5 

1.44 

705.2 

84%

5821 

40.3 

928.9 

4811 

6.3 

1.53 

770.6 

87%

6143 

43.9 

1011.1 

4935 

6.1 

1.62 

836.4 

90%

6448 

47.4 

1090.9 

5047 

5.9 

1.70 

899.4 

100%

7124 

55.2 

1270.0 

5261 

5.6 

1.88 

1035.0 

*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 65% throttle, for reference only.
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