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Evaluation of Low-Density Ablative TPS based on the foaming technique

  • Jaesung Shin*
  • , Jin Woo Yi
  • , Moon Won Song
  • *Corresponding author for this work
  • Korea Aerospace Research Institute
  • Korea Institute of Materials Science

Research output: Contribution to conferenceConference paperpeer-review

Abstract

A low-density ablative thermal protection system(TPS) was developed using a foaming(blowing) agent, and its performance was evaluated through arc-jet testing and post-analysis. The specimen with 0.36 g/cc was made within several tens of minutes. Arc-jet testing of the specimen yielded a recession rate of 0.524 mm/s, which is more than twice that of the reference model, Phenolic Impregnated Carbon Ablator(PICA). This high recession rate is attributed to the characteristics of the manufacturing process, which results in weak bonding between carbon fibers and subsequent spallation. Cross-section of the tested specimen showed clear evidence of phase change, with only a small portion of virgin. However, due to the small size of the specimen, one-dimensional heat conduction cannot be assumed, which likely led to an overestimation of the phase change location.

Original languageEnglish
Title of host publicationIAF Materials and Structures Symposium - Held at the 76th International Astronautical Congress, IAC 2025
Pages351-355
Number of pages5
ISBN (Electronic)9798331329365
DOIs
StatePublished - 2025
Event2025 IAF Materials and Structures Symposium at the 76th International Astronautical Congress, IAC 2025 - Sydney, Australia
Duration: 2025.09.292025.10.3

Publication series

NameProceedings of the International Astronautical Congress, IAC
Volume1-F219392
ISSN (Print)0074-1795

Conference

Conference2025 IAF Materials and Structures Symposium at the 76th International Astronautical Congress, IAC 2025
Country/TerritoryAustralia
CitySydney
Period25.09.2925.10.3

Keywords

  • Ablator
  • PICA
  • Re-entry
  • Thermal Protection System

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