5814915
doi
10.2514/6.2022-1308
oai:zenodo.org:5814915
user-retalt
user-eu
Charbonnier, Dominique
Destinus SA, Payerne, Switzerland,
Marwege, Ansgar
DLR Institute of Aerodynamics and Flow Technology, Supersonic and Hypersonic Technologies, 51147 Cologne, Germany
Guelhan Ali
DLR Institute of Aerodynamics and Flow Technology, Supersonic and Hypersonic Technologies, 51147 Cologne, Germany
Laureti, Mariasole
DLR Institute of Aerodynamics and Flow Technology, 37073 Göttingen, Germany
Karl, Sebastian
DLR Institute of Aerodynamics and Flow Technology, 37073 Göttingen, Germany
Aerodynamic investigations of a Vertical Landing Launcher configuration by means of Computational Fluid Dynamics and Wind Tunnel Tests
Vos, Jan
CFS Engineering, EPFL Innovation Park - Bat. A, 1015 Lausanne, Switzerland
info:eu-repo/semantics/openAccess
Creative Commons Attribution 4.0 International
https://creativecommons.org/licenses/by/4.0/legalcode
<p>In the RETALT (Retro Propulsion Assisted Landing Technologies) project critical technologies for two different vertical landing launcher configurations are investigated. For RETALT1, a Two Stage To Orbit launcher, only the first stage will be recovered using retro propulsion. A large number of wind tunnel experiments have been carried out at DLR in Cologne, while CFD simulations were made by CFS Engineering and DLR in Göttingen. This paper provides a detailed comparison of Wind Tunnel Experiments with CFD calculations in the hypersonic regime, with and without retro propulsion.</p>
Zenodo
2022-01-05
info:eu-repo/semantics/conferencePaper
5814914
user-retalt
user-eu
award_title=Retro Propulsion Assisted Landing Technologies; award_number=821890; award_identifiers_scheme=url; award_identifiers_identifier=https://cordis.europa.eu/projects/821890; funder_id=00k4n6c32; funder_name=European Commission;
1656933749.875059
6921395
md5:563e60c7811161a927e7c3b2bbdfa5a3
https://zenodo.org/records/5814915/files/6.2022-1308.pdf
public