KDE-UAS85UVC electronic speed controller
Also known as: KDEUAS85UVC, KDE UAS85UVC, KDE-UAS-85-UVC, KDE UAS 85 UVC, KDE Direct KDE-UAS85UVC, KDE Direct KDEUAS85UVC

KDE-UAS85UVC is an electronic speed controller that regulates electrical power supplied to a brushless propulsion motor. Continuous power is 4405 W. It links the propulsion motor to its power source and flight-control command path in an aircraft installation.
Description
KDE-UAS85UVC is an 85 A electronic speed controller (ESC) from KDE Direct, part of its UAS UVC series for brushless motors in multirotor and other unmanned aircraft. It controls the power fed to a brushless propulsion motor, accepting a throttle command from the flight controller and returning telemetry over CAN.
The controller is intended for commercial and industrial multirotor platforms operated in harsh environments, where its IP66 ingress protection and rugged aluminum 6061-T6 case allow all-weather operation. It has an internal 32-bit MCU, a proprietary control algorithm with dynamic advance timing from 12 to 30 degrees and an adaptive refresh rate of 50 to 600 Hz, with startup tuned for smooth motor synchronization.
For the integrator the main figures are as follows. The supply range is 14.8 V (4S LiPo) to 60.9 V (14S LiHV). Continuous current is 85 A for 180 s and peak current is 175 A for 5 s, which corresponds to a maximum continuous power of 4,405 W and a peak power of 9,065 W for 5 s. The maximum speed is 360,000 rpm electrical (2-pole). Mass is 110 g, or 150 g with wires and bullet connectors, and the size is 46 mm wide by 71 mm long. Continuous ratings require airflow of at least 5 mph across the heatsink; an overtemperature protection limits maximum rpm until the temperature falls, and the maximum case temperature is 95 degrees C.
Interfaces: the control lead is opto-isolated and the CAN bus port is not isolated. The PWM input has an automatic recognition algorithm and is factory calibrated. CAN telemetry supports KDECAN and DroneCAN and reports voltage, current, temperature, throttle and electrical rpm; data are logged to onboard EEPROM and downloaded through a micro-USB connection, with the KDE Direct Device Manager used for programming. There is no internal BEC, so a separate supply is needed for the flight controller and peripherals. The power leads are 12 AWG, the motor leads 13 AWG and the control lead 22 AWG, and the maximum DC wire length is 12 inches before added capacitance is needed.
Operating features include regenerative braking, temperature-controlled synchronous rectification, active monitoring of voltage, current, temperature and stall, an active anti-spark circuit to protect connectors and automatic throttle calibration. The maker states that the product is not NDAA compliant, which matters for buyers with procurement restrictions.
Specifications
| General | |
|---|---|
| Grade | Professional |
| Market | Civil |
| Platform class | Small UAS (<25 kg), Large UAS (25–150 kg) |
| Airframe | Multirotor |
| Availability | In production |
| Mass | 110 g[1] |
| Dimensions (L × W × H, mm) | 46 mm W x 71 mm L[1] |
| Waterproofness (IP rating) | IP66[1] |
| Key specifications | |
| Continuous current | 85 A[1] |
| Peak current | 175 A[1] |
| Supply voltage | 14.8 – 60.9 V[1] |
| Protocols | DroneCAN, Proprietary[1] |
| Additional specifications | |
| Continuous power | 4.405 kW[1] |
| Cooling | Forced air[1] |
| Physical interfaces | CAN, USB, PWM[1] |
| Telemetry | Live CAN telemetry and EEPROM logging: voltage, current, temperature, throttle and electrical RPM.[1] |
| BEC output | No internal BEC.[1] |
| Certifications and compliance | |
| Certifications | IP66 |
Sources
- kdedirect.com/products/kde-uas85uvc · checked October 25, 2026
A value without a number has no recorded source yet: we are adding it.
Frequently asked questions
What is the operating voltage range for the KDE-UAS85UVC?
The ESC is compatible with power systems ranging from 4S LiPo to 14S LiHV.
What is the ingress protection rating of the ESC?
The ESC has an IP66 certification for all-weather operation.
Reviews & Ratings
– / 5
No reviews yet. Be the first to rate.
Rate this product
Almost done: send the form below to publish your rating.
Thank you: your review is published and already counts in the rating.
Demo mode: the form is not connected yet and nothing was sent.
More products from KDE Direct
- FeaturedPropellers
KDE-CF305-DP carbon fiber propeller blades, 30.5 x 9.7 in, dual edition (CW/CCW)
- Diameter
- 774.7 mm
- Blade count
- 2
- Pitch type
- Fixed
- FeaturedPropellers
KDE-CF275-DP carbon fiber propeller blades, Dual-Edition (CW/CCW pair)
- Diameter
- 698.5 mm
- Blade count
- 2
- Pitch type
- Fixed
FeaturedESCsKDE-UAS95HVC 95 A HV multi-rotor electronic speed controller
- Continuous current
- 95 A
- Peak current
- 165 A
- Supply voltage
- 11.1 – 52.2 V
- FeaturedElectric motors
KDE7215XF-135 brushless electric motor for heavy-lift multirotor UAS
- Continuous power
- 2.915 kW
- Supply voltage
- 22.2 – 60.9 V
- Grade
- Professional
Alternative products
Featured
Featured
FeaturedESCsHigh-voltage ESCs electronic speed controller
- Grade
- Professional
- Market
- Dual-use
- Availability
- In production
- Featured
Related news

Safran turbojets to power Falcon supersonic UAV target
Falcon is a reusable supersonic uncrewed aerial target for missile-defense training, and its propulsion is the subject of a partnership between Safran Power Units and UVAD Technologies. Safran supplies two turbojet engines, and flight…

Honeywell tests 1 MW hybrid-electric generator for airship
Honeywell Aerospace tests a 1 MW generator in a Mexicali test cell, and Flying Whales will integrate it into the hybrid-electric powertrain of its LCA60T airship. The unit reaches 1 MW steady state at 97% efficiency, giving…

Honeywell HON1600 small turbine engine targets USAF CCA
Honeywell Aerospace presents the HON1600, a small turbine engine it positions for the US Air Force's Collaborative Combat Aircraft (CCA) program, after a core engine run in September 2025. The Air Force has issued a request for proposals…
This product listing is maintained by our editorial team and may contain errors. Last updated .



















