Mission Success Requires Better Engines
The NW-230 offers 18 horsepower and heavy-fuel versatility for Group III aircraft
Most UAV engines fail because they weren't designed for the mission. The NW-230 is different. This American-made, twin-cylinder engine provides a dedicated solution for aircraft weighing between 90 and 160 kg. It replaces fragile, modified hobby components with a rugged, 230cc architecture that prioritizes stay-time and minimal maintenance. By building on the combat-tested lineage of the NW-44 and NW-88, Northwest UAV created a system that works as hard as the platforms it powers.
Performance is worthless if it isn't predictable. The NW-230 uses electronic fuel injection to ensure reliable cold starts and consistent operation at altitudes up to 36,000 feet. It produces up to 18 horsepower while weighing1 only 10 kg, offering a power-to-weight ratio that translates directly into larger payloads and faster cruise speeds. This is a tool for professionals who need hardware to perform every time the wheels leave the ground.
NW-230 Features
The NW-230 is built for reliability. Depending on configuration and options, the horsepower range is 15-182 with a 230 cc displacement, weighing 10 kg ± 200 grams1. Based on the combat-proven NW-88 and NW-44.
- Fuel Flexibility3: Runs on gasoline or heavy logistics fuels like JP-5, JP-8, and Jet-A.
- Maximum Uptime: Engineered for a +500-hour overhaul cycle to keep your fleet operational.
- Onboard Power: Integrated alternator options provide up to 3kW for demanding sensor suites.
- Predictive Care: Live telemetry monitoring identifies maintenance needs before they become failures.
- Stealthy Operation: Features a lightweight, quiet muffler to reduce acoustic signatures.
- Expert Support: Every engine includes technical assistance and aerospace-compliant manufacturing standards.
- Export Classification: EAR99.
NOTE: Actual performance will vary depending on PMU configuration, application, propeller, fuel type, oil, environmental conditions, type of operation, direction of rotation, generator losses, and cowling configuration. 1Weight does not include Generator, Generator Controller/Rectifier, or Propeller. Includes: ECU, Muffler, Engine Mount, ACHT, and Engine Harness. | 2Depending on propeller/RPM. | 3Fuel is subject to regional and seasonal variations. The user is responsible for testing, validating, and defining operational limits with their local gasoline source.
Engine application is dependent on airframe factors including: Aerodynamics, propeller, and operational concept. Please contact NWUAV for guidance.