Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Jean-Marc BOUILLY"'
Autor:
Adriana STEFAN, Gheorghe IONESCU, George PELIN, Cristina-Elisabeta PELIN (BAN), Ion DINCA, Beatriz PEREZ, Sonia FLOREZ, Jorge BARCENA, Konstantina MERGIA, Kostoula TRIANTOU, Christian ZUBER, Waldemar ROTAERMEL, Jean-Marc BOUILLY, Gregory PINAUD, Wolfgang FISCHER
Publikováno v:
INCAS Bulletin, Vol 6, Iss 4, Pp 87-101 (2014)
A hybrid thermal protection system for atmospheric earth re-entry based on ablative materials on top of ceramic matrix composites is investigated for the protection of the metallic structure in oxidative and high temperature environment of the space
Externí odkaz:
https://doaj.org/article/b3b3f2ff835049968c9505bc54ce426e
Publikováno v:
In The Journal of Space Safety Engineering June 2024 11(2):198-210
Autor:
Jean-Marc Bouilly, Wolfgang Fischer, Iñaki Garmendia, Beatriz Pérez, Konstatina Mergia, K. Triantou, J. Barcena, Gregory Pinaud, S. Florez
Publikováno v:
Acta Astronautica. 134:85-97
A new thermal protection system for atmospheric earth re-entry is proposed. This concept combines the advantages of both reusable and ablative materials to establish a new hybrid concept with advanced capabilities. The solution consists of the design
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::362eee7bd1528ee5ac8ba753e3844a62
https://doi.org/10.1016/j.actaastro.2017.01.045
https://doi.org/10.1016/j.actaastro.2017.01.045
Publikováno v:
AIAA Scitech 2019 Forum
AIAA Scitech 2019 Forum, Jan 2019, San Diego, United States. ⟨10.2514/6.2019-2234⟩
AIAA Scitech 2019 Forum, Jan 2019, San Diego, United States. ⟨10.2514/6.2019-2234⟩
International audience; While the number of artificial space object re-enter the Earth atmosphere daily, predicting the reentry of a space debris remains an open problem. The reentry prediction is a multi-physics problem involving aerodynamics comput
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::98f38de8eb0cc70725241b2a4823cb7d
https://hal.science/hal-02392632
https://hal.science/hal-02392632
Breakup prediction under uncertainty: Application to upper stage controlled reentries from GTO orbit
Publikováno v:
Aerospace Science and Technology
Aerospace Science and Technology, 2019, ⟨10.1016/j.ast.2019.02.031⟩
Aerospace Science and Technology, Elsevier, 2019, ⟨10.1016/j.ast.2019.02.031⟩
Aerospace Science and Technology, 2019, ⟨10.1016/j.ast.2019.02.031⟩
Aerospace Science and Technology, Elsevier, 2019, ⟨10.1016/j.ast.2019.02.031⟩
More and more human-made space objects re-enter the atmosphere, and yet the risk for human populations remains often unknown because predicting their reentry trajectories is formidably complex. While falling back on Earth, the space object absorbs la
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::db36415fa79d5d6d7181a55f101e41f7
http://hdl.handle.net/20.500.12278/9066
http://hdl.handle.net/20.500.12278/9066
Autor:
Dominique Bernard, Beatriz Pérez, Christian Zuber, Konstantina Mergia, Cristina Ban, S. Florez, Georg Herdrich, George Vekinis, Vincent Leroy, Bartomeu Massuti, Gheorghe Ionescu, Waldermar Rotaermel, G. Pinaud, Agnes de Montbrun, Michel Descomps, Adriana Stefan, K. Triantou, Pedro Portela, J. Barcena, Ing Hermann Hald, Jean-Marc Bouilly, Wolfgang Fischer
The FP7 project HYDRA addresses the development of a hybrid thermal protection solution, where a low density ablator is attached on top of a thermo-structural ceramic core by means of the use of high temperature adhesives. The project aims to design,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0824471b11b4af0d6ca25dc67adbeb1b
http://hdl.handle.net/11556/380
http://hdl.handle.net/11556/380
Autor:
Stefanos Fasoulas, Pénélope Leyland, Tobias Hermann, Lionel Marraffa, Stefan Löhle, Jean-Marc Bouilly
Plasma wind tunnel experiments have been performed simulating a Hayabusa reentry trajectory point at 78.8 km altitude with a velocity of 11.7 km/s corresponding to a local mass–specific enthalpy of 68.4 MJ/kg and a stagnation pressure of 2.44 kPa.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::30c2f929dc83c9b7a6a43aa620ac129f
https://infoscience.epfl.ch/record/230719
https://infoscience.epfl.ch/record/230719