Zobrazeno 1 - 10
of 25
pro vyhledávání: '"Nestoridi, Maria"'
Autor:
Zhang, Ningxin, Beutl, Alexander, Rajinovic, Kristijan, Kahr, Jürgen, Jahn, Marcus, Nestoridi, Maria
Publikováno v:
In Journal of Energy Storage March 2023 59
Autor:
Nestoridi, Maria
In this thesis aluminium alloys containing small additions of both tin (~ 0.1 wt %) and gallium (~ 0.05 wt %) dissolve anodically at high rates in brine media; at room temperature, current densities > 0.2 A cm-2 can be obtained at potentials close to
Externí odkaz:
https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.509552
Autor:
Nestoridi Maria, Barde Henri
Publikováno v:
E3S Web of Conferences, Vol 16, p 08005 (2017)
Lithium-ion (Li-ion) batteries are established as the state of the art [1] rechargeable batteries for terrestrial and space applications today since the launch of Proba 1 satellite in 2001. [2] At the moment there is strong interest by all stakeholde
Externí odkaz:
https://doaj.org/article/aacf59fb190c48eeb888bfde29ef9455
Autor:
Bard Frederic, Carré Aurore, Fernandez Pablo, Nestoridi Maria, Alia Sergio, Datta Aakesh, Durodola Olabisi
Publikováno v:
E3S Web of Conferences, Vol 16, p 13005 (2017)
This paper presents the IOV and FOC Battery in orbit trend analysis and degradation modelling based on the Galileo experience in the frame of the ESPC 2016. Galileo provides a unique opportunity to study a constellation of satellites in the Medium Ea
Externí odkaz:
https://doaj.org/article/551f65a6533545769e25a5bd935ac14a
Publikováno v:
E3S Web of Conferences, Vol 16, p 17009 (2017)
In the frame of an ESA GSTP 5.2 activity (contract 4000105105), the qualification and life testing of a Saft range of Li-ion batteries based on VES16 cells and theirs autonomous simplified balancing system (SBS) has been carried out. In this abstract
Externí odkaz:
https://doaj.org/article/3ab9689acb5b42c4a9e0d5e816de274d
Publikováno v:
E3S Web of Conferences, Vol 16, p 08006 (2017)
The battery energy density remains a key parameter accounting for the satellite mass budget. As illustration to this, the rechargeable battery still represents 100 to 200 of kilograms for a typical Eurostar 3000 satellite, which can represent up to 5
Externí odkaz:
https://doaj.org/article/7dcdb4424bf0467985f82f50bd7c6fa5
Publikováno v:
E3S Web of Conferences, Vol 16, p 07002 (2017)
Saft recently designed, developed and qualified in the frame of Research and Development contract (GSTP-5) with the European Space Agency (ESA) three new VES16 batteries: 8S4P (4 parallel strings of 8 cells in series), 10S5P, 10S16P [ 1 ]. In order t
Externí odkaz:
https://doaj.org/article/71cde130d722451e92e72c34f95d69a5
Autor:
Bausier François, Nestoridi Maria, Samaniego Bruno, Simola Juhani, Wolahan Andrew, Austin Julian, Soares Tiago
Publikováno v:
E3S Web of Conferences, Vol 16, p 13002 (2017)
Due to the increasing risk posed on satellites from space debris, requirements are now being implemented into satellites to be launched in the future to prevent the release of additional debris. One of the key requirements is the electrical passivati
Externí odkaz:
https://doaj.org/article/ec1422f2d13640db96cc531742107eef
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