TY - GEN
T1 - Evaluation of Low-Density Ablative TPS based on the foaming technique
AU - Shin, Jaesung
AU - Yi, Jin Woo
AU - Song, Moon Won
N1 - Publisher Copyright:
Copyright © 2025 by the International Astronautical Federation (IAF). All rights reserved.
PY - 2025
Y1 - 2025
N2 - 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.
AB - 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.
KW - Ablator
KW - PICA
KW - Re-entry
KW - Thermal Protection System
UR - https://www.scopus.com/pages/publications/105036068821
U2 - 10.52202/083088-0037
DO - 10.52202/083088-0037
M3 - Conference paper
AN - SCOPUS:105036068821
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 351
EP - 355
BT - IAF Materials and Structures Symposium - Held at the 76th International Astronautical Congress, IAC 2025
T2 - 2025 IAF Materials and Structures Symposium at the 76th International Astronautical Congress, IAC 2025
Y2 - 29 September 2025 through 3 October 2025
ER -