Low-cost turbojet engine with 1300 kg-f of thrust for Destinus E and Destinus G. Reduced weight and lower mechanical complexity than competitors.

Specifications

Max thrust: 1300 kg-f (dry)

2200 kg-f (reheat)

Fuel consumption (max thrust): < 0.95 kg/kg-f*h

Mass: < 150 kg

Dimensions: Ø 460x1200mm

Compressor: 8-stage axial flow

Combustors: annular combustion chamber

Turbine: 2-stage axial flow

Cooling: bleed air