Abstract
With an increasing level of complexity in aerospace missions, a high-fidelity model of material response model is needed. It also becomes clear that the volatile chemical species that evolved during the ablation can alter the performance of the Thermal Protection System as well as the outer flow field. In this work, the pyrolysis gas is modeled as a non-equilibrium multi-species gas mixture instead of a bulk gas. The proposed gas model is based on the experimental data based on the pyrolysis of Phenolic Impregnated Carbon Ablator (PICA). The generation of non-equilibrium gas will also have an impact on the boundary layer flows since each gas component will be coupled and react with the external flow. In the final version of this study, we believe the proposed model can provide a higher level of confidence in the material response analysis when a new atmosphere is considered.
Original language | English |
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Title of host publication | AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023 |
DOIs | |
State | Published - 2023 |
Event | AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023 - San Diego, United States Duration: Jun 12 2023 → Jun 16 2023 |
Publication series
Name | AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023 |
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Conference
Conference | AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023 |
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Country/Territory | United States |
City | San Diego |
Period | 6/12/23 → 6/16/23 |
Bibliographical note
Publisher Copyright:© 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
Funding
Funding for this work was provided by NASA Award 80NSSC18K0261 (SpaceTech-REDDI-2017 - ESI) as well as NASA ACCESS STRI award No: 80NSSC21K1117.
Funders | Funder number |
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NASA | 80NSSC18K0261 |
ESI Group | 80NSSC21K1117 |
ASJC Scopus subject areas
- Energy Engineering and Power Technology
- Nuclear Energy and Engineering
- Aerospace Engineering