81-08 G2 integrated motor and ESC propulsion module

The 81-08 G2 module combines a propulsion motor, position sensing and an electronic speed controller. Its sensored control supports reversible operation and braking, with motor winding and module configuration selected for the aircraft installation.
Description
The 81-08 Module is an integrated motor and ESC propulsion module from Vertiq with an integrated controller. The 81-08 G2 module, part number VERT-M28.1-E16.1, is an integrated motor and ESC propulsion module from Vertiq. It is a brushless electric motor of the 81-08 size with a speed constant of 85 Kv, combined with a 14S, 60 A continuous electronic speed controller and a position sensor in one unit, designed for drone propulsion and robotics.
The module is intended to drive propeller loads on multirotors and other electric aircraft. Because the position is sensed, the controller works without desync, supports 3D reversible operation without delay at zero crossing and can run at any speed from -4900 RPM to 4900 RPM. Regenerative and active braking, active freewheeling and coast modes are available, and the motor is backdrivable. An optional multi-turn angle firmware adds a position controller with a minimum-jerk trajectory generator, and anticogging is available on request.
Three nested controllers can be selected: an integrated PID velocity controller with a second order polynomial feed forward, which suits propellers, a voltage controller that compensates for varying battery voltage and a raw PWM controller. For the integrator, the voltage controller keeps thrust consistent as the battery discharges, and the velocity controller gives a stable response without a separate flight-controller loop.
The main figures are a torque constant of 0.112 N m/A, a motor resistance of 0.202 ohm (0.219 ohm including the controller) at 25 °C, a pulsed current of 50 A for 100 ms, a no-load speed of 139.4 rad/s and a no-load current of 0.4 A at 15 V. The mass is 292 g in the base configuration and 313 g in the default configuration, both without wires. The recommended supply is 12 V to 60 V, corresponding to 4S to 14S batteries, with caution above 12S, and regenerated energy must not exceed the voltage limit, so the built-in regeneration limiter or an external load is needed. The recommended ambient temperature is -20 °C to 50 °C, and the controller reduces performance as it approaches its limits.
For integration, the communication protocols are DroneCAN, DShot (150 to 1200), 1-2 ms PWM, serial UART with access to control parameters, Oneshot and Multishot. The connector board carries up to two CAN connections wired to the same bus, power pads, RX/TX pads and three GPIOs. The mounting uses M4 and M3 threaded holes. The module can be shipped without the stator cover and connector board, so wire exits and IP ratings up to IP56 can be defined by the customer.
Protection functions include over-current, over-voltage, over-speed and over-temperature protection, motor health monitoring, standard and custom telemetry, and a safe arming procedure.
Specifications
| General | |
|---|---|
| Grade | Professional[1] |
| Market | Dual-use |
| Platform class | Small UAS (<25 kg), Large UAS (25–150 kg) |
| Airframe | Multirotor, Fixed-wing, Hybrid VTOL, Tiltrotor/tiltwing |
| Availability | In production |
| Additional specifications | |
| Integrated controller | Yes[1] |
| Physical interfaces | CAN, PWM, UART[1] |
Sources
- vertiq.co/s/VERT-M281-E161-Vertiq_81-08_85Kv_datasheet.pdf · checked October 19, 2026
A value without a number has no recorded source yet: we are adding it.
Frequently asked questions
What is the maximum supply voltage for the 81-08 G2 propulsion module?
The absolute maximum supply voltage for the module is 80 V.
What is the mass of the module in its default configuration?
The mass of the module in the default configuration, excluding wires and accessories, is 313 grams.
What is the recommended operating ambient temperature range?
The recommended ambient temperature range for operation is -20 to 50 degrees Celsius.
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 Vertiq
FeaturedElectric motors40-14 G2 integrated motor and ESC module
- Grade
- Professional
- Market
- Dual-use
- Availability
- In production
FeaturedElectric motors60-08 G2 integrated drone propulsion module
- Grade
- Professional
- Market
- Dual-use
- Availability
- In production
FeaturedElectric motors81-08 G2 integrated motor and ESC propulsion module
- Grade
- Professional
- Market
- Dual-use
- Availability
- In production
FeaturedElectric motors60-08 G2 integrated drone propulsion module
- Grade
- Professional
- Market
- Civil
- Availability
- In production
Alternative products
FeaturedElectric motorsHeliStorm electric rotorcraft motor
- Continuous power
- 221 kW
- Peak power
- 324 kW
- Supply voltage
- 520 – 820 V
Featured
FeaturedElectric motorsHPDM-350 integrated electric motor drive
- Continuous power
- 350 kW
- Power-to-weight ratio
- 7 kW/kg
- Grade
- Professional
FeaturedElectric motorsHPDM-30 integrated electric motor drive
- Continuous power
- 33 kW
- Power-to-weight ratio
- 8 kW/kg
- Grade
- Professional
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 .


















