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Aerodynamic investigations of a Vertical Landing Launcher configuration by means of Computational Fluid Dynamics and Wind Tunnel Tests

Vos, Jan and Charbonnier, Dominique and Marwege, Ansgar and Gülhan, Ali and Laureti, Mariasole and Karl, Sebastian (2022) Aerodynamic investigations of a Vertical Landing Launcher configuration by means of Computational Fluid Dynamics and Wind Tunnel Tests. In: AIAA Aviation 2022 Forum. AIAA SciTech Forum, 2022-01-03 - 2022-01-07, San Diego, CA, USA. doi: 10.2514/6.2022-1308.

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Official URL: https://doi.org/10.2514/6.2022-1308

Abstract

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.

Item URL in elib:https://elib.dlr.de/188192/
Document Type:Conference or Workshop Item (Speech)
Title:Aerodynamic investigations of a Vertical Landing Launcher configuration by means of Computational Fluid Dynamics and Wind Tunnel Tests
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Vos, JanCFS Engineeringhttps://orcid.org/0000-0003-1525-943XUNSPECIFIED
Charbonnier, DominiqueCFS Engineeringhttps://orcid.org/0000-0002-9600-9258UNSPECIFIED
Marwege, AnsgarUNSPECIFIEDhttps://orcid.org/0000-0002-3912-9114UNSPECIFIED
Gülhan, AliUNSPECIFIEDhttps://orcid.org/0000-0001-7460-0576UNSPECIFIED
Laureti, MariasoleUNSPECIFIEDhttps://orcid.org/0000-0001-5887-004XUNSPECIFIED
Karl, SebastianUNSPECIFIEDhttps://orcid.org/0000-0002-5558-6673UNSPECIFIED
Date:5 January 2022
Journal or Publication Title:AIAA Aviation 2022 Forum
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI:10.2514/6.2022-1308
Status:Published
Keywords:RETALT, CFD, Wind Tunnel Tests, Aerodynamics, Retro Propulsion
Event Title:AIAA SciTech Forum
Event Location:San Diego, CA, USA
Event Type:international Conference
Event Start Date:3 January 2022
Event End Date:7 January 2022
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Reusable Space Systems and Propulsion Technology
Location: Göttingen , Köln-Porz
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology
Institute for Aerodynamics and Flow Technology > Spacecraft, GO
Deposited By: Marwege, Ansgar
Deposited On:22 Nov 2022 09:25
Last Modified:24 Apr 2024 20:49

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  • Aerodynamic investigations of a Vertical Landing Launcher configuration by means of Computational Fluid Dynamics and Wind Tunnel Tests. (deposited 22 Nov 2022 09:25) [Currently Displayed]

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