50cc single-cylinder heavy-fuel UAV engine, 3.6 hp, ~340 g/kWh, FlexDI™ integrated
50cc single-cylinder heavy-fuel UAV engine, 3.6 hp, ~340 g/kWh, FlexDI™ integrated
75cc single-cylinder heavy-fuel UAV engine, 5.1 hp, ~345 g/kWh, FlexDI™ integrated
150cc opposed twin-cylinder heavy-fuel UAV engine, 11.9 hp, <340 g/kWh, MIL-STD-810H qualified
350cc opposed twin-cylinder heavy-fuel UAV engine, 28.4 hp, ~325 g/kWh, Group 3 capable
UAV power management system with dual 28 V outputs, alternator/battery/shore auto-switching, and CANbus telemetry
UAV engine management system with black-box logging, fault monitoring, anti-stall, and CAN communication
Air-assisted direct fuel injection system atomising to ~8 µm droplets for heavy-fuel UAV engines
Advanced variant engine management system with improved fuelling algorithms under electrical load and black-box logging
In-house engine and propeller simulation platform for UAV performance optimisation across altitudes and environments
Orbital remote-start device integrated with the PMS for UAV engine ground operations