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Aerothermal analysis of the RETPRO flight configuration

Laureti, Mariasole and Karl, Sebastian and Bykerk, Tamas and Kirchheck, Daniel (2024) Aerothermal analysis of the RETPRO flight configuration. In: 9th Edition of the 3AF International Conference on Space Propulsion 2024, pp. 1-11. 9th Edition of the 3AF International Conference on Space Propulsion 2024, 2024-05-20 - 2024-05-23, Glasgow, Scotland.

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Official URL: https://www.3af-spacepropulsion.com/

Abstract

the RETPRO (Validation of Wind Tunnel Test and CFD Techniques for Retro-propulsion) project, part of ESA´s Future Launchers Preparatory Programme (FLPP), aims to investigate launch system reusability technologies using wind tunnel testing and computational fluid dynamics (CFD). This paper describes and summarizes the CFD based aerothermal load predictions for a Vertical Take-off Vertical Landing (VTVL) reusable launcher configuration during the retropropulsion phase. An analysis of representative numerical results, obtained for the case Mach 5.3 and three active engines, is provided with the aim to show typical flow field phenomena and the resulting heating patterns occurring on the launcher surface. Parametric studies are performed to evaluate the effect of the number of operating engines, thrust vector control and different fuels (hydrocarbon vs. hydrogen).

Item URL in elib:https://elib.dlr.de/198838/
Document Type:Conference or Workshop Item (Speech)
Title:Aerothermal analysis of the RETPRO flight configuration
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Laureti, MariasoleUNSPECIFIEDhttps://orcid.org/0000-0001-5887-004XUNSPECIFIED
Karl, SebastianUNSPECIFIEDhttps://orcid.org/0000-0002-5558-6673UNSPECIFIED
Bykerk, TamasUNSPECIFIEDhttps://orcid.org/0000-0001-8662-3484163310987
Kirchheck, DanielUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:May 2024
Journal or Publication Title:9th Edition of the 3AF International Conference on Space Propulsion 2024
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-11
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
UNSPECIFIED3AFUNSPECIFIEDUNSPECIFIED
Status:Published
Keywords:CFD, aerothermal loads, supersonic retro-propulsion, reusable launchers
Event Title:9th Edition of the 3AF International Conference on Space Propulsion 2024
Event Location:Glasgow, Scotland
Event Type:international Conference
Event Start Date:20 May 2024
Event End Date:23 May 2024
Organizer:3AF
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 > Spacecraft, GO
Institute for Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology
Deposited By: Laureti, Mariasole
Deposited On:10 Jul 2024 09:00
Last Modified:10 Jul 2024 09:00

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