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Outflow characterization of a transpiration cooled fin for the sounding rocket experiment HIFLIER 1

Peichl, Jonas Stefan and Di Martino, Giuseppe and Selzer, Markus (2025) Outflow characterization of a transpiration cooled fin for the sounding rocket experiment HIFLIER 1. HiSST: 4th International Conference on High-Speed Vehicle Science & Technology, 2025-09-22 - 2025-09-26, Tours, Frankreich.

Full text not available from this repository.

Abstract

This paper presents a study on the outflow characteristics of a sharp edged, transpiration cooled fin as flown as part of the FinEx experiment of the HIFLIER1 sounding rocket. The permeable ceramic matrix composite material used for the transpiration cooled leading edge shows in general a relatively homogeneous outflow pattern disrupted by significant strong jets caused by small inhomgeneities. The general strongly anisotropic outflow characteristics were also investigated. The findings of the outflow characterization led to valuable insights for the design of future sharp edged transpiration cooled structures

Item URL in elib:https://elib.dlr.de/216926/
Document Type:Conference or Workshop Item (Speech)
Title:Outflow characterization of a transpiration cooled fin for the sounding rocket experiment HIFLIER 1
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Peichl, Jonas StefanUNSPECIFIEDhttps://orcid.org/0009-0002-7115-8369UNSPECIFIED
Di Martino, GiuseppeUNSPECIFIEDhttps://orcid.org/0000-0002-2338-4778UNSPECIFIED
Selzer, MarkusUNSPECIFIEDhttps://orcid.org/0000-0003-1081-5281UNSPECIFIED
Date:September 2025
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Transpiration Cooling, Ceramic Matrix Composites, Thermal Protection Systems
Event Title:HiSST: 4th International Conference on High-Speed Vehicle Science & Technology
Event Location:Tours, Frankreich
Event Type:international Conference
Event Start Date:22 September 2025
Event End Date:26 September 2025
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: Stuttgart
Institutes and Institutions:Institute of Structures and Design > Space System Integration
Deposited By: Peichl, Jonas Stefan
Deposited On:13 Nov 2025 16:28
Last Modified:13 Nov 2025 16:28

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