MAD 5010 EEE Drone Motor Specifications
Motor Model
|
MAD 5010 EEE V2.0
|
Number of pole pairs
|
14 |
Stator
|
Anticorrosive
|
Varnished wire Degree
|
180C |
Motor Size
|
D:56 32.7 mm
|
Magnet Degree
|
150C
|
Degree of Protection
|
Rain protection |
Cable Length
|
150 mm 16# Awg(Black) silicone
|
Centrifugal Heat Dissipation
|
Independent |
Rotor Balance
|
5 mg
|
Propeller Mounting Holes
|
D:12 M32, D:18 M32
|
Motor Balance
|
10 mg
|
Shaft Diameter
|
IN: 5 mm
|
Motor Mounting Holes
|
D:25 M34, D:30 M34 |
| Bearing |
EZO 685ZZ*1 / 695ZZ*1
|
Disruptive test
|
500 V |
MAD 5010 EEE 200KV
| Nominal Voltage |
6-12S lipo battery |
| No Load Current |
0.69A / 20V |
| Product Boxed Weight |
323g (110 x 110 x 50 mm) |
| Recommended ESC |
AMPX PRO 40A (2~6S) |
| Recommended Propellers |
16×5.4, 17×5.8, 22×6.6, 22×7.0, 24×7.2 |
| UAV take-off weight |
12S-17″/7kg–Quadcopter |
|
10.5kg–Hexacopter 14kg–Octocopter |
| Single rotor take-off weight |
1.5kg ~ 2kg |
MAD 5010 EEE 240KV
| Nominal Voltage |
6S lipo battery |
| No Load Current |
0.76A / 20V |
| Internal resistance |
94.6m |
| Product Boxed Weight |
322g (110 x 110 x 50 mm) |
| Recommended ESC |
MAD AMPX PRO 40A (2~6S) |
| Recommended Propellers |
20×6.0, 21×6.3, 22×6.6, 22×7.0 |
| UAV take-off weight |
6S-22″/5kg–Quadcopter |
|
7.5kg–Hexacopter 10kg–Octocopter |
| Single rotor take-off weight |
1.5kg ~ 2kg |
MAD 5010 EEE 310KV
| Nominal Voltage |
6S lipo battery |
| No Load Current |
1.25A / 20V |
| Product Boxed Weight |
324g (110 x 110 x 50 mm) |
| Recommended ESC |
MAD AMPX PRO 40A (2~6S) |
| Recommended Propellers |
20×6.0, 21×6.3, 22×6.6, 22×7.0 |
| UAV take-off weight |
6S-20″/7kg–Quadcopter |
|
10.5kg–Hexacopter 14kg–Octocopter |
| Single rotor take-off weight |
2kg ~ 2.5kg |
MAD 5010 EEE 370KV
| Nominal Voltage |
6S lipo battery |
| No Load Current |
1.56A / 20V |
| Product Boxed Weight |
324g (110 x 110 x 50 mm) |
| Recommended ESC |
MAD AMPX PRO 40A (2~6S) |
| Recommended Propellers |
17×5.8, 18×6.1, 18×5.7 |
| UAV take-off weight |
6S-18″/7.2kg–Quadcopter |
|
10.8kg–Hexacopter 14.4kg–Octocopter |
| Single rotor take-off weight |
1.7kg ~ 2.2kg |
MAD 5010 EEE is designed to carry payloads of 8002900g per rotor, with 14-22″carbon propeller. Support 6S-12S. Max thrust of single rotor is up to 4400g, unit motor only weighs 158g. EEE reduction version design, minimized weight, optimized efficiency and flight time extended.
* Open body design for better passive heat dissipation.* Propeller installation compatibility.
* Reduced motor weight.
* Motor mounting holes standarization.
Motor Test Benchmarks
Products Packaging
Company Profile
FAQ
Certifications
Reviews
There are no reviews yet.