MAD 5010 EEE Drone Motor Specifications
Motor Model |
MAD 5010 EEE V2.0 |
Number of pole pairs |
14 | ||||||
Stator |
Anticorrosive |
Varnished wire Degree |
180°C | ||||||
Motor Size |
D:56 × 32.7 mm |
Magnet Degree |
150°C |
||||||
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 M3×2, D:18 M3×2 |
Motor Balance |
≤10 mg |
||||||
Shaft Diameter |
IN: 5 mm |
Motor Mounting Holes |
D:25 M3×4, D:30 M3×4 | ||||||
Bearing | EZO 685ZZ*1 / 695ZZ*1 |
Disruptive test |
500 V |
MAD 5010 EEE 200KV
Specifications |
---|
RPM/V | 200 KV |
Nominal Voltage | 6-12S lipo battery |
No Load Current | 0.69A / 20V |
Internal resistance | 106mΩ |
Motor Weight | 162.9 g |
Product Boxed Weight | 323g (110 x 110 x 50 mm) |
Maximum Current | 22.3 A |
Maximum Power | 1029 W |
Maximum thrust | 5.2 kg |
Maximum Torque | 1.09 Nm |
Recommended ESC | AMPX PRO 40A (2~6S) |
AMPX 40A (5-14S) HV |
Recommended Propellers | 16x5.4, 17x5.8, 22x6.6, 22x7.0, 24x7.2 |
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
Specifications |
---|
RPM/V | 240 KV |
Nominal Voltage | 6S lipo battery |
No Load Current | 0.76A / 20V |
Internal resistance | 94.6mΩ |
Motor Weight | 161 g |
Product Boxed Weight | 322g (110 x 110 x 50 mm) |
Maximum Current | 28.9 A |
Maximum Power | 681W |
Maximum thrust | 4.1 kg |
Maximum Torque | 1.23 Nm |
Recommended ESC | MAD AMPX PRO 40A (2~6S) |
Recommended Propellers | 20x6.0, 21x6.3, 22x6.6, 22x7.0 |
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
Specifications |
---|
RPM/V | 310 KV |
Nominal Voltage | 6S lipo battery |
No Load Current | 1.25A / 20V |
Internal resistance | 51mΩ |
Motor Weight | 162 g |
Product Boxed Weight | 324g (110 x 110 x 50 mm) |
Maximum Current | 46.8 A |
Maximum Power | 991W |
Maximum thrust | 5.2 kg |
Maximum Torque | 1.4 Nm |
Recommended ESC | MAD AMPX PRO 40A (2~6S) |
Recommended Propellers | 20x6.0, 21x6.3, 22x6.6, 22x7.0 |
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
Specifications |
---|
RPM/V | 370 KV |
Nominal Voltage | 6S lipo battery |
No Load Current | 1.56A / 20V |
Internal resistance | 38mΩ |
Motor Weight | 162.2 g |
Product Boxed Weight | 324g (110 x 110 x 50 mm) |
Maximum Current | 44 A |
Maximum Power | 1019W |
Maximum thrust | 4.9 kg |
Maximum Torque | 1.12 Nm |
Recommended ESC | MAD AMPX PRO 40A (2~6S) |
Recommended Propellers | 17x5.8, 18x6.1, 18x5.7 |
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 800–2900g 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.
* Reduced motor weight.
* Motor mounting holes standarization.