Zobrazeno 1 - 10
of 31
pro vyhledávání: '"Eva Anglada"'
Autor:
Iñaki Garmendia, Eva Anglada
Publikováno v:
Aerospace, Vol 9, Iss 12, p 821 (2022)
Ground thermal tests are always mandatory before any space mission is flown into space. The collected results of these tests are mainly temperatures of the different parts of the spacecraft (nodes) for different mission scenarios. The measured temper
Externí odkaz:
https://doaj.org/article/0ec0f45e47dd43ef819111e6c715a0cb
Publikováno v:
Journal of Manufacturing and Materials Processing, Vol 6, Iss 6, p 164 (2022)
The high cooling rates reached during metal additive manufacturing (MAM) generate microstructures very different from those obtained by other conventional manufacturing methods. Therefore, research about the modeling of this type of microstructure is
Externí odkaz:
https://doaj.org/article/fec4aa836bc246f9848cdef9150dd2f1
Publikováno v:
Aerospace, Vol 9, Iss 3, p 126 (2022)
In this paper, the design and validation of a heat storage device based on phase change materials are presented, with the focus on improving the thermal control of micro-satellites. The main objective of the development is to provide a system that is
Externí odkaz:
https://doaj.org/article/57dd7e35d90b4921a16cad9df076c3b6
Publikováno v:
Metals, Vol 11, Iss 11, p 1747 (2021)
Simulation is a very useful tool in the design of the part and process conditions of high-pressure die casting (HPDC), due to the intrinsic complexity of this manufacturing process. Usually, physics-based models solved by finite element or finite vol
Externí odkaz:
https://doaj.org/article/b1f0a73361b54a639de29845d625fac9
Publikováno v:
Metals, Vol 10, Iss 8, p 1071 (2020)
The use of optimization algorithms to adjust the numerical models with experimental values has been applied in other fields, but the efforts done in metal casting sector are much more limited. The advances in this area may contribute to get metal cas
Externí odkaz:
https://doaj.org/article/ac71e0a3c41147ba9f8ec615898eb055
Publikováno v:
International Journal of Aerospace Engineering, Vol 2017 (2017)
The correlation of the thermal mathematical models (TMMs) of spacecrafts with the results of the thermal test is a demanding task in terms of time and effort. Theoretically, it can be automatized by means of optimization techniques, although this is
Externí odkaz:
https://doaj.org/article/e44c1e96efe24c9d9a362d4979b4a955
Autor:
Iñaki Garmendia, Eva Anglada
Publikováno v:
TECNALIA Publications
Fundación Tecnalia Research & Innovation
Fundación Tecnalia Research & Innovation
There are always differences between the computer predicted temperatures of a spacecraft thermal model and the temperatures measured during the mandatory laboratory thermal tests. As a consequence, the model must be correlated before the spacecraft i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d047253c8387b782aff9b38da24a3de6
https://doi.org/10.1016/j.actaastro.2022.07.014
https://doi.org/10.1016/j.actaastro.2022.07.014
Publikováno v:
Journal of Manufacturing and Materials Processing; Volume 6; Issue 6; Pages: 164
The high cooling rates reached during metal additive manufacturing (MAM) generate microstructures very different from those obtained by other conventional manufacturing methods. Therefore, research about the modeling of this type of microstructure is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::75d99db014b1d01ab8b3d768639740a2
Publikováno v:
Aerospace; Volume 9; Issue 3; Pages: 126
Addi. Archivo Digital para la Docencia y la Investigación
Universidad de Cantabria (UC)
TECNALIA Publications
Fundación Tecnalia Research & Innovation
instname
Addi. Archivo Digital para la Docencia y la Investigación
Universidad de Cantabria (UC)
TECNALIA Publications
Fundación Tecnalia Research & Innovation
instname
In this paper, the design and validation of a heat storage device based on phase change materials are presented, with the focus on improving the thermal control of micro-satellites. The main objective of the development is to provide a system that is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1a5a9497ad4ecc8b7fe08479205e1684
Autor:
Eva Anglada, Iñaki Garmendia
Temperatures predicted by the Thermal Mathematical Models (TMMs) used in the thermal control design of spacecraft, usually present differences with the values measured during the thermal test campaign. Therefore, the TMMs must be correlated with the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::967d2501a52ae578bb75d1d1d21c1d32
http://hdl.handle.net/11556/1237
http://hdl.handle.net/11556/1237
