Dario Severino

- Senior System Engineer for HP3 Martian Instrument (in behalf of DLR) for NASA mission InSight - Project Manager of the mechanical department in AST GmbH - Bid Manager for ESA ITTs and Industrial proposals - Project Manager of thermal vacuum technologies - Lead designer

Quality Manager (Eurocopter) System engineer for Fuel cells (Airbus)

Define the working process: data classification, operative phase, delivery phase of the analysis process and plan the workload. - Data architecture in terms of ATA, suppliers, kind of manufacturing and component - Identify critical WB spare parts to support the Airbus A340 service fleet - Select a new supply base, made of a limited number of suppliers specialized in spare parts activity - Secure availability of spare parts Database management. VB script to extract and manage data from Taksy.

Management of the opto-mechanical Budgets and requirements for APMI facility, using innovative EUV lithography with extreme ultraviolet light. - Mirror deformation (SFD)  Parasitic Forces and Moments  Bonding effects on the mirror  Mounting Metrology  Screw mounting effects - Mirror positioning - Motion of the mirror (Ranges)

Project Control: Estimate manpower load, budget, and project time schedule. Project Manager: Convert customer needs into technical specifications. Development of a system design solution according cost, schedule, performance and risk. Verification that technical solution satisfy customer requirements; Configuration controlling; Define of design constraints; Customer Support. Development of space ground equipment and flight test facilities; CATIA, FEM design and LabVIEW programming. Quality Management.

Concept and installation team for wiring harness and electrical components. CATIA V4; Taksy; Zamiz and Enovia VPM

Fortran programming; Trajectories/performance analysis of VEGA launcher evolution. Configuration Launcher and Mass Budget Management. Solide propulsion system performance analysis.

Development of experimental facility to study advanced heat pipes in microgravity conditions; Assembly, Integration and Test; Data analysis and comparison; CFD thermal analysis software (Fluent and gambit) is used to compare experimental results. 45th ESA Parabolic Flight Campaign with "Ultra-light weight flexible radiator with micro heat pipes" experiment, in collaboration with A.I.S.T. (Japan), University of Tokyo (Japan), M.A.R.S. Center (Italy). Data analysis manager.

Mission Analysis; Launchers and Ground Base

CFD; Space Systems; Microgravity; Flight Dynamics; aerodynamics; space propulsion;Thermal and Mechanical analysis; celestial mechanics; space structures