Associate Professor in Experimental AerodynamicsUniversity of Twente, Enschede, Niederlande
Life Cycle Assessment (LCA) framework for quantification of environmental im-pacts rocket launches and re-entryPaul Scherrer Institute (PSI), Villigen, Schweiz
Analysis of a methodology for global effects of launchers on the atmosphere and environmentUniversity of Stuttgart (US), Stuttgart, Deutschland
Missionisation of re-entry and recovery architectures for upper stagesDeimos Engineering and Systems S.L.U. (DES), Madrid, Spanien
Multidisciplinary system-level trade-offs w.r.t. environmental impact for reusable first stagesOffice national d’études et de recherches aérospatiales (ONERA), Paris, Frankreich
Multi fidelity, multi-disciplinary optimisation for sustainable rocket-based launcher systemsUniversity of Strathclyde (UOS), Glasgow, Großbritannien
Assessing the environmental sustainability of future launchers with respect to different systems architectures and operating scenariosPolitecnico di Torino (POLITO), Turin, Italien
Studying the impacts of rocket upper stage and satellite re-entry using laboratory experiments and chemistry-climate modellingUniversity of Leeds (UL), Leeds, Großbritannien
Modelling of rocket impacts on atmospheric composition, dynamics, and climatePhysikalisch-Meteorologisches Observatorium Davos and World Radiation center (PMOD), Davos, Schweiz
Global atmospheric model simulations and sub-grid plume parameterizationInstitut Pierre-Simon Laplace (IPSL), Paris, Frankreich
Large eddy simulation of the nozzle flow and interaction with ambient airCentre Euopéen de Recherche et de Formation Avancée en Calcul Scientifique (CERFACS), Toulouse, Frankreich
Evolution of the rocket engine exhaust plume along the flight trajectoryechnische Universität Dresden (TUD), Dresden, Deutschland
Evolution of ablation induced emissions during re-entry phaseTechnische Universität Dresden (TUD), Dresden, Deutschland
Experimental investigation of ablation products from gas-surface interaction during re-entriesUniversity of Stuttgart (US), Stuttgart, Deutschland
Numerical modelling of ablation products resulting from upper stage re-entriesUniversité libre de Bruxelles (ULB), Brüssel, Belgien
End of life emissions of composite materials upon re-entryEcole Polytechnique Fédérale de Lausanne (EPFL), Lausanne, Schweiz
Generation of experimental data for validating numerical modelling of launcher engine exhaust chemical composition in ground tests of CH4/O2 thrust chambersDeutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Hardthausen, Deutschland
Development of a chemical reduction schemeUniversité libre de Bruxelles (ULB), Brüssel, Belgien
Numerical study of the impact of operative conditions on combustion emissionsInstitut Superieur de l’Aeronautique et de l’Espace (ISAE), Toulouse, Frankreich
