- Hitec D131MW 8.5mm, Ultra-Nano, Coreless, Metal Case, Low Profile, Wing Servo
- Features high-efficiency coreless motor and dual ball bearings
- Offers powerful torque in a nano package
- Compatible with 1-2 cell LiPo and fully programmable
- Boasts a durable metal case and IP4X dust/water resistance
- Ideal for high-performance, thin-wing aircraft and gliders
The Hitec D131MW 8.5mm, Ultra-Nano, Coreless, Metal Case, Low Profile, Wing Servo is a competitively positioned servo that boasts a low profile and a machined aluminum case. It is equipped with a high-efficiency coreless motor and dual ball bearings, making it one of the most durable and longest-lasting servos in its category. This robust technology is ideally suited for pilots and drivers who require powerful torque in a nano package. It is particularly effective for high-performance, thin-wing aircraft and hand-launch gliders.
The D131MW is associated with the ultra-performance and reliability that Hitec is known for, and its quality engineering, enduring power, and precision are sure to impress discerning modelers.
This servo features a wide operating voltage, compatibility with 1-2 cell LiPo, a coreless motor, durable metal gears, an all-aluminum case, dual ball bearings, high response, high-resolution circuitry, and smart sense technology for servo analytics. It also offers full programmability with Hitec's DPC11 or HFP-30.
The performance specifications of this servo include an operating voltage range of 4.8 ~ 7.4 V, a speed of 0.11 @ 7.4V, a maximum torque range of 40 @ 7.4V, and a current draw at idle of 30mA @ 7.4V. It also has a no-load operating current draw of 110 mA @ 7.4V, a stall current draw of 900 mA @ 7.4V, and a dead band width of 2μs.
Physically, the servo measures 0.87 x 0.34 x 0.91 inches and weighs 0.35 ounces. It features a 32-bit programmable digital circuit type, a brushless motor type, 5 metal gear materials, 2 ball bearings, an M25T output shaft, and an aluminum case material. It is also IP4X rated for dust and water resistance.
