reuSable strAtegic space Launcher Technologies & Operations

Project Information

SALTO

Grant agreement ID: 101082007

DOI

10.3030/101082007

EC signature date 2 December 2022

Start date 1 December 2022

End date 30 September 2026

Funded under

• Digital, Industry and Space

Total cost

€ 42 805 477,06

EU contribution

€ 39 000 000,00

Coordinated by

ARIANEGROUP SAS
France

CORDIS provides links to public deliverables and publications of HORIZON projects.

Links to deliverables and publications from FP7 projects, as well as links to some specific result types such as dataset and software, are dynamically retrieved from OpenAIRE .

Publications

Conference proceedings (8)

Building an aerodynamic model of a vertical landing reusable launcher based on CFD and wind tunnel experiments in SALTO and CFD4SALTO

Author(s): 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
Publisher: 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

Author(s): M. Laureti, German Aerospace Center (DLR e.V.), Germany S. Karl, German Aerospace Center (DLR e.V.), Germany
Publisher: Zenodo
DOI: 10.5281/ZENODO.17200335

Development and manufacturing of a landing leg system for reusable launchers T(hemis)3 in the SALTO project

Author(s): Christoph Thies, MT Aerospace Peter Ortmann, MT Aerospace Carl S Modén Thomas Zenker
Publisher: Researchgate

Scalability of aerodynamics from demonstrator to full flight scale of a vertical landing reusable launcher

Author(s): 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
Publisher: Zenodo
DOI: 10.5281/ZENODO.17200016

Parametric grid fin design study for the T3 vehicle within SALTO

Author(s): Jens Neumann, DLR
Publisher: DGLR STAB – Symposium 2024

Flight dynamics evaluation for the T3 suborbital flight test

Author(s): 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.
Publisher: Zenodo
DOI: 10.5281/ZENODO.17200107

Autonomous Flight Safety System: Embedded Software and Hardware Equipment for NewSpace Ground and Onboard Safety

Author(s): Alejandro Sabán, Eduard Diez, Manel Soria, Miquel Sureda
Published in: IAF Space Operations Symposium, 2025, ISBN 9798331312183
Publisher: International Astronautical Federation (IAF)
DOI: 10.52202/078367-0071

Analysis of unsteady pressure loads on the Themis T3 vehicle in unpropelled backward flight

Author(s): Tim Horchler, German Aerospace Center (DLR e.V.), Germany Mariasole Laureti, German Aerospace Center (DLR e.V.), Germany
Publisher: Zenodo
DOI: 10.5281/ZENODO.17200246

Intellectual Property Rights

Registered design (1)

Tuile amovible en PAEK imprimé 3D pour fixer liège sur plaque métal

Application/Publication number: SOLEAU 2023-04
Date: 2023-12-04
Applicant(s): ID-SERVICES