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Characterization of ablator recession and thermal response using non-intrusive techniques

Salvi, Ciro und Hohn, Oliver und Gülhan, Ali (2026) Characterization of ablator recession and thermal response using non-intrusive techniques. AIAA Journal. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J065731. ISSN 0001-1452.

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Kurzfassung

The main goal of this study is the investigation of the recession augmentation of cork-based ablators in particle-laden Martian flow environment in the arc-heated facility L2K. The thermal response of the P50 cork-based ablator is assessed through recession and material temperature measurements. An innovative laser-based technique was employed to measure the in situ, time-resolved evolution of material thickness due to ablation, swelling, and erosion. The results were compared with 3D surface scans. Sample temperatures were monitored using infrared thermography and embedded thermocouples. In the tests, a slightly simplified Martian atmosphere (97% CO2 and 3% N2) was used. The high-enthalpy flow was loaded with micrometric magnesium oxide particles moving at approximately 2000 m/s. Flow conditions without particles were also studied for comparison. The particle-induced erosion was evaluated by comparing conditions with and without particles. In the presence of particles, the increased surface recession causes higher in-depth temperature due to material thinning. For this reason, the design of cork-based heat shields for Martian missions around dust storms requires increased safety factors.

elib-URL des Eintrags:https://elib.dlr.de/219062/
Dokumentart:Zeitschriftenbeitrag
Titel:Characterization of ablator recession and thermal response using non-intrusive techniques
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Salvi, Cirociro.salvi (at) dlr.dehttps://orcid.org/0000-0002-4185-1042202276534
Hohn, OliverOliver.Hohn (at) dlr.dehttps://orcid.org/0000-0002-4225-7352NICHT SPEZIFIZIERT
Gülhan, Aliali.guelhan (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:2026
Erschienen in:AIAA Journal
Referierte Publikation:Ja
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Ja
DOI:10.2514/1.J065731
Verlag:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0001-1452
Status:veröffentlicht
Stichwörter:Arc-heated wind tunnel, Cork-based ablator, Ablation, Recession, Swelling, Erosion, LPT, P50, Infrared thermography, Temperature
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:keine Zuordnung
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R - keine Zuordnung
DLR - Teilgebiet (Projekt, Vorhaben):R - keine Zuordnung
Standort: Köln-Porz
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik > Über- und Hyperschalltechnologien, KP
Hinterlegt von: Salvi, Ciro
Hinterlegt am:13 Jan 2026 13:29
Letzte Änderung:13 Jan 2026 13:29

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