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

Salvi, Ciro and Hohn, Oliver and 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.

Full text not available from this repository.

Abstract

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.

Item URL in elib:https://elib.dlr.de/219062/
Document Type:Article
Title:Characterization of ablator recession and thermal response using non-intrusive techniques
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Salvi, CiroUNSPECIFIEDhttps://orcid.org/0000-0002-4185-1042202276534
Hohn, OliverUNSPECIFIEDhttps://orcid.org/0000-0002-4225-7352UNSPECIFIED
Gülhan, AliUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2026
Journal or Publication Title:AIAA Journal
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI:10.2514/1.J065731
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0001-1452
Status:Published
Keywords:Arc-heated wind tunnel, Cork-based ablator, Ablation, Recession, Swelling, Erosion, LPT, P50, Infrared thermography, Temperature
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:other
DLR - Research area:Raumfahrt
DLR - Program:R - no assignment
DLR - Research theme (Project):R - no assignment
Location: Köln-Porz
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology
Deposited By: Salvi, Ciro
Deposited On:13 Jan 2026 13:29
Last Modified:13 Jan 2026 13:29

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