Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Joffrey Coheur"'
Publikováno v:
International Journal for Uncertainty Quantification, Vol. 13, no.2, p. 53-80 (2023)
For space missions involving atmospheric entry, a thermal protection system is essential to shield the spacecraft and its payload from the severe aerothermal loads. Carbon/phenolic composite materials have gained renewed interest to serve as ablative
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e2856403b11019e03756d9f830351766
https://hdl.handle.net/2078.1/271592
https://hdl.handle.net/2078.1/271592
Autor:
Thierry Magin, Francisco Torres-Herrador, Nagi N. Mansour, Philippe Chatelain, Joffrey Coheur, Maarten Arnst
Publikováno v:
Journal of Materials Science. 56:6845-6860
This paper provides the analytical solution to a one-parameter Šesták–Berggren kinetic model for the thermoanalytical study of pyrolysis reactions involving multiple independent parallel reactions. Such multiple independent parallel reactions are
Autor:
Thierry Magin, Andreas Eschenbacher, Julien Blondeau, Francisco Torres-Herrador, Joffrey Coheur, Kevin Van Geem
Publikováno v:
Aerospace Science and Technology
AEROSPACE SCIENCE AND TECHNOLOGY
AEROSPACE SCIENCE AND TECHNOLOGY
Thermal Protection Materials (TPM) such as carbon/phenolic composites are used to protect spacecraft structures from extreme conditions. This protection is, in part, achieved by the decomposition via pyrolysis of the phenolic resin. Finite rate chemi
Autor:
Francesco Panerai, Nagi N. Mansour, Francisco José Torres Herrador, Julien Blondeau, Jeremie B. E. Meurisse, Thierry Magin, Jean Lachaud, Joffrey Coheur
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d85c795d58b932b4203454e6f11fed5e
https://hdl.handle.net/20.500.14017/24756f0d-b20d-4c31-b15d-3a46b6b593a2
https://hdl.handle.net/20.500.14017/24756f0d-b20d-4c31-b15d-3a46b6b593a2
Autor:
Francisco Torres-Herrador, Thierry Magin, Julien Blondeau, Francesco Panerai, Nagi N. Mansour, Joffrey Coheur, Maarten Arnst
Publikováno v:
Aerospace Science and Technology. 100:105784
Carbon/phenolic ablators are successfully used as thermal protection material for spacecraft. Nevertheless, their complex thermal degradation is not yet fully understood, and current pyrolysis models do not reproduce important features of available e
Publikováno v:
47th AIAA Thermophysics Conference.