The maximum continuous power mode of 160 kW is available up to 2,000 m, even at high temperatures. The turboshaft engine can be started even at cold temperatures below -30 °C without preheating.
The engine is equipped with an autonomous oil and fuel system, BLDC electric starter-generator and a digital engine control unit (ECU). The ECU controls the acceleration and deceleration of the gas generator to maintain a constant output shaft speed. The ECU also provides subsequent automatic cooling of hot components after the engine stops.
Turboshaft engine can be controlled by an analogue interface (control voltage) or digital interface (based on CAN Aerospace V1.7 protocol). The engine parameters for a multi-function cockpit display are only available in digital format. Two engine versions are available: PBS TS100ZA 5,978 RPM with or PBS TS100DA with 2,158 RPM (output shaft speed).
Standard accessories (included):
digital control system (ECU), ignition, connecting cable
electromagnetic fuel valve, boost pump, oil cooler
alternator, control box, EMS display, thermostatic valve, and others
Look at Turbine engines brochure here.