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dc.contributor.author | Torres-Herrador, F. | es_ES |
dc.contributor.author | Leroy, V. | es_ES |
dc.contributor.author | Helber, B. | es_ES |
dc.contributor.author | Contat-Rodrigo, L | es_ES |
dc.contributor.author | Lachaud, J. | es_ES |
dc.contributor.author | Magin, T. | es_ES |
dc.date.accessioned | 2023-07-10T18:03:17Z | |
dc.date.available | 2023-07-10T18:03:17Z | |
dc.date.issued | 2020-09 | es_ES |
dc.identifier.issn | 0001-1452 | es_ES |
dc.identifier.uri | http://hdl.handle.net/10251/194800 | |
dc.description.abstract | [EN] A multicomponent kinetic mechanism has been developed for the pyrolysis at low heating rate of carbon/ phenolic thermal protection material and a wood species. An experimental campaign has been carried out using thermogravimetric analysis to study the mass loss under different conditions of crucible (with or without a lid) and heating rate for both materials. Using a pierced lid to cover the crucible during pyrolysis promotes char production compared with the case of open crucible. Kinetic parameters were then extracted from the experiments by an optimization approach using an in-house-developed kinetic identification code. The parameters recovered for the two applications allow to reproduce accurately the mass loss evolution. | es_ES |
dc.description.sponsorship | The research of F. T.-H., V. L., and T. E. M. is sponsored by the European Research Council Proof of Concept Grant #713726. The samples of the ablator studied in this project were provided through the European Space Agency (ESA) Research Program ABLARADABLA project #ESA ITTAO/1-7987/14/NL/RA. Niaouli samples were provided through the European Research Council Proof ofConcept Grant #713726. We would like to thank Gregory Pinaud (ArianeGroup) for his suggestions on the fitting algorithm. Gertjan Glabeke von Karman Institute (VKI) is acknowledged for his support during the experimental campaign. Christian Zuber and Thomas Reimer (German Aerospace Center [DLR] Stuttgart) are acknowledged for providing characterization support and information regarding the production of ZURAM (R). | es_ES |
dc.language | Inglés | es_ES |
dc.publisher | American Institute of Aeronautics and Astronautics | es_ES |
dc.relation.ispartof | AIAA Journal | es_ES |
dc.rights | Reserva de todos los derechos | es_ES |
dc.subject.classification | MAQUINAS Y MOTORES TERMICOS | es_ES |
dc.title | Multicomponent Pyrolysis Model for Thermogravimetric Analysis of Phenolic Ablators and Lignocellulosic Biomass | es_ES |
dc.type | Artículo | es_ES |
dc.identifier.doi | 10.2514/1.J059423 | es_ES |
dc.relation.projectID | info:eu-repo/grantAgreement/ESA//ITTAO/1-7987%2F14/NL%2FRA/EU | |
dc.relation.projectID | info:eu-repo/grantAgreement/EC/H2020//713726/EU | |
dc.rights.accessRights | Abierto | es_ES |
dc.contributor.affiliation | Universitat Politècnica de València. Escuela Técnica Superior de Ingeniería del Diseño - Escola Tècnica Superior d'Enginyeria del Disseny | es_ES |
dc.description.bibliographicCitation | Torres-Herrador, F.; Leroy, V.; Helber, B.; Contat-Rodrigo, L.; Lachaud, J.; Magin, T. (2020). Multicomponent Pyrolysis Model for Thermogravimetric Analysis of Phenolic Ablators and Lignocellulosic Biomass. AIAA Journal. 58(9):4081-4089. https://doi.org/10.2514/1.J059423 | es_ES |
dc.description.accrualMethod | S | es_ES |
dc.relation.publisherversion | https://doi.org/10.2514/1.J059423 | es_ES |
dc.description.upvformatpinicio | 4081 | es_ES |
dc.description.upvformatpfin | 4089 | es_ES |
dc.type.version | info:eu-repo/semantics/publishedVersion | es_ES |
dc.description.volume | 58 | es_ES |
dc.description.issue | 9 | es_ES |
dc.relation.pasarela | S\436872 | es_ES |
dc.contributor.funder | European Research Council | es_ES |
dc.contributor.funder | European Space Agency | |
dc.contributor.funder | European Commission |