06 Fakultät Luft- und Raumfahrttechnik und Geodäsie

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    Icy ocean worlds - astrobiology research in Germany
    (2024) Klenner, Fabian; Baqué, Mickael; Beblo-Vranesevic, Kristina; Bönigk, Janine; Boxberg, Marc S.; Dachwald, Bernd; Digel, Ilya; Elsaesser, Andreas; Espe, Clemens; Funke, Oliver; Hauber, Ernst; Heinen, Dirk; Hofmann, Florence; Hortal Sánchez, Lucía; Khawaja, Nozair; Napoleoni, Maryse; Plesa, Ana-Catalina; Postberg, Frank; Purser, Autun; Rückriemen-Bez, Tina; Schröder, Susanne; Schulze-Makuch, Dirk; Ulamec, Stephan; de Vera, Jean-Pierre Paul
    Icy bodies with subsurface oceans are a prime target for astrobiology investigations, with an increasing number of scientists participating in the planning, development, and realization of space missions to these worlds. Within Germany, the Ocean Worlds and Icy Moons working group of the German Astrobiology Society provides an invaluable platform for scientists and engineers from universities and other organizations with a passion for icy ocean worlds to share knowledge and start collaborations. We here present an overview about astrobiology research activities related to icy ocean worlds conducted either in Germany or in strong collaboration with scientists in Germany. With recent developments, Germany offers itself as a partner to contribute to icy ocean world missions.
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    Manufacture and thermomechanical characterization of wet filament wound C/C‐SiC composites
    (2021) Frieß, Martin; Böyükbas, Muhammed; Vogel, Felix; Cepli, Daniel; Schatz, Oliver; Süß, Fabia; Shi, Yuan
    The paper presents manufacture of C/C‐SiC composite materials by wet filament winding of C fibers with a water‐based phenolic resin with subsequent curing via autoclave as well as pyrolysis and liquid silicon infiltration (LSI). Almost dense C/C‐SiC composite materials with different winding angles ranging from ±15° to ±75° could be obtained with porosities lower than 3% and densities in the range of 2 g/cm3. Thermomechanical characterization via tensile testing at room temperature and at 1300°C revealed higher tensile strength at elevated temperature than at room temperature. Thus, C/C‐SiC material obtained by wet filament winding and LSI‐processing has excellent high‐temperature strength for high‐temperature applications. Crack patterns during pyrolysis, microstructure after siliconization, and tensile strength strongly depend on the fiber/matrix interface strength and winding angle. Moreover, calculation tools for composites, such as classical laminate and inverse laminate theory, can be applied for structural evaluation and prediction of mechanical performance of C/C‐SiC structures.