MAD 5008 EEE V2.0 Drone Motor Overview
5008 as the first motor was designed and developed by MAD EU in 2015. the result never let the motor designer and user disappointed. It is the most efficient motor equipped with 18-20inch propeller. the best option for the multirotor need 1-2kg/rotor.It is widely used for the long-range inspection drone mapping drone surveying drone quadcopter hexcopter mulitirotor.
MAD 5008 EEE V2.0 Drone Motor Specifications
| Specification
|
Motor Model
|
MAD 5008 EEE V2.0
|
Number of pole pairs
|
14 |
Stator
|
Anticorrosive
|
Varnished wire Degree
|
180C |
Motor Size
|
D:56 30.7 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 5008 EEE V2.0 Motor Data
| Motor Data |
|
|
| Motor Model |
MAD 5008 EEE V2.0 |
Number of pole pairs |
| Stator |
TAIWAN / Anticorrosive |
Varnished wire Degree |
| Motor Size |
D:56 30.7 mm |
Magnet Degree |
| Degree of Protection |
Rain protection |
Cable Length |
| Centrifugal Heat Dissipation |
Independent |
Rotor Balance |
| Propeller Mounting Holes |
D:12 M32. D:18 M32 |
Motor Balance |
| Shaft Diameter |
IN: 5 mm |
Motor Mounting Holes |
| Bearing |
EZO 685ZZ1 / 695ZZ1 |
Disruptive test |
| Additional Accessories |
Propeller Plate 1. 4-6 Adapter Ring 1. 3.5mm Bullet Connector3. Heat Shrinkable Tube3. M3*8mm 4 Motor Screws. M310mm 2 Propeller Screws. Sticker2 |
|
MAD 5008 EEE V2.0 170KV
| Specifications |
|
| RPM/V |
170 KV |
| Nominal Voltage |
12S lipo battery |
| No Load Current |
0.42A / 20V |
| Internal resistance |
195m |
| Motor Weight |
130 g |
| Product Boxed Weight |
293g (110 x 110 x 50 mm) |
| Maximum Current |
20.6 A |
| Maximum Power |
981W |
| Maximum thrust |
4.8 kg |
| Maximum Torque |
1.09 Nm |
| Recommended ESC |
MAD AMPX 40A (5-14S) HV |
| Recommended Propellers |
17×5.8. 18×6.1. 18×5.7 |
| UAV take-off weight |
12S-18″/7kg–Quadcopter |
|
10.5kg–Hexacopter 14kg–Octocopter |
| Single rotor take-off weight |
1.5kg ~ 2kg |
MAD 5008 EEE 240KV
| Nominal Voltage |
6S lipo battery |
| No Load Current |
0.67A / 20V |
| Product Boxed Weight |
294g (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. 18×6.1 |
| UAV take-off weight |
6S-21″/5kg–Quadcopter |
|
7.5kg–Hexacopter 10kg–Octocopter |
| Single rotor take-off weight |
1kg ~ 2kg |
MAD 5008 EEE 300KV
| Nominal Voltage |
6S lipo battery |
| No Load Current |
0.99A / 20V |
| Product Boxed Weight |
290g (110 x 110 x 50 mm) |
| Recommended ESC |
MAD AMPX PRO 40A (2~6S) |
| Recommended Propellers |
18×6.1. 18×5.7. 19×5.7. 20×6.0 |
| UAV take-off weight |
6S-18″/5kg–Quadcopter |
|
7.5kg–Hexacopter 10kg–Octocopter |
| Single rotor take-off weight |
1kg ~ 2kg |
MAD 5008 EEE 340KV
| Nominal Voltage |
6S lipo battery |
| No Load Current |
1.1A / 20V |
| Internal resistance |
66.4m |
| Product Boxed Weight |
290g (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. 19×5.7 |
| UAV take-off weight |
6S-18″/6kg–Quadcopter |
|
9kg–Hexacopter 12kg–Octocopter |
| Single rotor take-off weight |
1.5kg ~ 2kg |
MAD 5008 EEE 400KV
| Nominal Voltage |
6S lipo battery |
| No Load Current |
1.35A / 20V |
| Internal resistance |
44.5m |
| Product Boxed Weight |
301g (110 x 110 x 50 mm) |
| Recommended ESC |
MAD AMPX PRO 40A (2~6S) |
| Recommended Propellers |
16×5.4. 17×5.8 |
| UAV take-off weight |
6S-17″/7kg–Quadcopter |
|
10.5kg–Hexacopter 14kg–Octocopter |
| Single rotor take-off weight |
1.5kg ~ 2kg |
MAD 5008 EEE Drone Motor for Endurance Flight
The MAD 5008 is designed to carry payloads of 7002500g per rotor. with 15-22 “carbon propeller. Support 6S~12S. Max thrust of single rotor is up to 3880g. unit motor only weighs 130g. EEE reduction version design. minimized weight. optimized efficiency and flight time extended.
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