Conference paper Open Access
Vos, Jan;
Charbonnier, Dominique;
Marwege, Ansgar;
Guelhan Ali;
Laureti, Mariasole;
Karl, Sebastian
{ "description": "<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>", "license": "https://creativecommons.org/licenses/by/4.0/legalcode", "creator": [ { "affiliation": "CFS Engineering, EPFL Innovation Park - Bat. A, 1015 Lausanne, Switzerland", "@id": "https://orcid.org/0000-0003-1525-943X", "@type": "Person", "name": "Vos, Jan" }, { "affiliation": "Destinus SA, Payerne, Switzerland,", "@id": "https://orcid.org/0000-0002-9600-9258", "@type": "Person", "name": "Charbonnier, Dominique" }, { "affiliation": "DLR Institute of Aerodynamics and Flow Technology, Supersonic and Hypersonic Technologies, 51147 Cologne, Germany", "@id": "https://orcid.org/0000-0002-3912-9114", "@type": "Person", "name": "Marwege, Ansgar" }, { "affiliation": "DLR Institute of Aerodynamics and Flow Technology, Supersonic and Hypersonic Technologies, 51147 Cologne, Germany", "@id": "https://orcid.org/0000-0003-4905-5881", "@type": "Person", "name": "Guelhan Ali" }, { "affiliation": "DLR Institute of Aerodynamics and Flow Technology, 37073 G\u00f6ttingen, Germany", "@id": "https://orcid.org/0000-0001-5887-004X", "@type": "Person", "name": "Laureti, Mariasole" }, { "affiliation": "DLR Institute of Aerodynamics and Flow Technology, 37073 G\u00f6ttingen, Germany", "@type": "Person", "name": "Karl, Sebastian" } ], "headline": "Aerodynamic investigations of a Vertical Landing Launcher configuration by means of Computational Fluid Dynamics and Wind Tunnel Tests", "image": "https://zenodo.org/static/img/logos/zenodo-gradient-round.svg", "datePublished": "2022-01-05", "url": "https://zenodo.org/record/5814915", "@context": "https://schema.org/", "identifier": "https://doi.org/10.2514/6.2022-1308", "@id": "https://doi.org/10.2514/6.2022-1308", "@type": "ScholarlyArticle", "name": "Aerodynamic investigations of a Vertical Landing Launcher configuration by means of Computational Fluid Dynamics and Wind Tunnel Tests" }
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