To assure low inert weight of propulsion stages, in many cases the use of a turbo pump feed system is advantageous. This is especially true, in case liquid propellant rocket engines are operating at pressures in excess of 30 bar, as the inert weight of pressure feed systems will increase significantly.

Our development is based on the philosophy, that only through implementation of technologies enabling series production, cost reduction can be achieved.

(60 kN LOX / LCH4 Turbo pump shown below.)