Building an aerodynamic model of a vertical landing reusable launcher based on CFD and wind tunnel experiments in SALTO and CFD4SALTO
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Autores:
Ansgar Marwege, German Aerospace Center (DLR e.V.), Germany Josef Klevanski, German Aerospace Center (DLR e.V.), Germany Junnai Zhai, German Aerospace Center (DLR e.V.), Germany Ali Gülhan, German Aerospace Center (DLR e.V.), Germany Jan Vos, CFS Engineer
Editor:
Zenodo
DOI:
10.5281/ZENODO.17199286
Aerothermal analysis of Themis T3: influence of nozzle cluster geometry on the base heating and heat loads on the grid fins
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Autores:
M. Laureti, German Aerospace Center (DLR e.V.), Germany S. Karl, German Aerospace Center (DLR e.V.), Germany
Editor:
Zenodo
DOI:
10.5281/ZENODO.17200335
Development and manufacturing of a landing leg system for reusable launchers T(hemis)3 in the SALTO project
Autores:
Christoph Thies, MT Aerospace Peter Ortmann, MT Aerospace Carl S Modén Thomas Zenker
Editor:
Researchgate
Scalability of aerodynamics from demonstrator to full flight scale of a vertical landing reusable launcher
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Autores:
Ansgar Marwege, German Aerospace Center (DLR e.V.), Germany Pawel Goldyn, German Aerospace Center (DLR e.V.), Germany Josef Klevanski, German Aerospace Center (DLR e.V.), Germany Ali Gülhan, German Aerospace Center (DLR e.V.), Germany
Editor:
Zenodo
DOI:
10.5281/ZENODO.17200016
Parametric grid fin design study for the T3 vehicle within SALTO
Autores:
Jens Neumann, DLR
Editor:
DGLR STAB – Symposium 2024
Flight dynamics evaluation for the T3 suborbital flight test
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Autores:
J. Gutiérrez Briceño, Deimos Engineering and Systems S.L.U. G. Medicil, Deimos Engineering and Systems S.L.U. A. Princil, Deimos Engineering and Systems S.L.U. G. De Zaiacomo, Deimos Engineering and Systems S.L.U.
Editor:
Zenodo
DOI:
10.5281/ZENODO.17200107
Autonomous Flight Safety System: Embedded Software and Hardware Equipment for NewSpace Ground and Onboard Safety
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Autores:
Alejandro Sabán, Eduard Diez, Manel Soria, Miquel Sureda
Publicado en:
IAF Space Operations Symposium, 2025, ISBN 9798331312183
Editor:
International Astronautical Federation (IAF)
DOI:
10.52202/078367-0071
Analysis of unsteady pressure loads on the Themis T3 vehicle in unpropelled backward flight
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Autores:
Tim Horchler, German Aerospace Center (DLR e.V.), Germany Mariasole Laureti, German Aerospace Center (DLR e.V.), Germany
Editor:
Zenodo
DOI:
10.5281/ZENODO.17200246