Concept generation means that the customer’s requirements are analyzed and transformed into the configuration of the future engine. It is a starting point of a long journey ending in the mandatory certification of the product.

Demands to the reliability, minimum takeoff weight, efficiency, service life and power (thrust) vary depending on the customer.

We specialize in the development of the following power plants for helicopters and airplanes:

• auxiliary power units (100-400 hp)
• turboshaft power plants (400-6000 hp) for helicopters with the maximum takeoff weight of 15 tons
• turboprop power plants (2000-6000 hp) for airplanes with the takeoff weight up to 24 tons
• turbojet power plants (1 -120 kN) for military airplanes including drones.

Principal requirements for engines and power plants:

• Efficiency, compact size and weight, easy maintenance
• Specific mass
• Reliability, long service life, efficiency of components
• Maximum specific thrust