Ludwigsburg, Baden-Württemberg, Germany
Design and Characterisation of Coaxial Swirl Injectors for the Application in a Throttleable Nitrous Oxide Ethanol Thruster
Responsible for the development of the propulsion system for a hybrid sounding rocket Design and construction of a 4000 N hybrid rocket engine Development and operation of a rocket engine test bench
Responsible for the thermal protection system of the combustion chamber and the rocket nozzle of a hybrid sounding rocket.
- Supervision of the tutorial for structural design in aeronautics and astronautics - FEM simulations of the mechanical loads during the quench of the superconductor in the AMS-100 magnetic space spectrometer.