Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Deger Akin"'
Thermal conductance of contacting surfaces is an important parameter for spacecraft thermal design. No universal model exists that can enable one to predict contact resistance between any two surfaces. If none of the available models fit the need for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5400a4de433c642bdffb580d6c799006
https://avesis.deu.edu.tr/publication/details/1e82f1d6-b323-4754-8a22-f6aa6933697b/oai
https://avesis.deu.edu.tr/publication/details/1e82f1d6-b323-4754-8a22-f6aa6933697b/oai
Publikováno v:
2013 6th International Conference on Recent Advances in Space Technologies (RAST).
Satellites are subjected to extensive (ground level) environmental testing before launch to ensure successful launch and on-orbit operation. While there exists three primary environmental tests i.e., thermal, structural and electromagnetic interferen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1685fdda6aa37715cc1ebd032f5c8091
https://doi.org/10.1109/rast.2013.6581268
https://doi.org/10.1109/rast.2013.6581268
Publikováno v:
2013 6th International Conference on Recent Advances in Space Technologies (RAST).
In this paper, specifications and capabilities of a newly built thermal vacuum chamber used for the system level thermal vacuum tests is presented. Thanks to the thermoregulation system, it is also possible to perform both subsystem and equipment lev
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f5cd045f5da79693b56b996889a95e56
https://doi.org/10.1109/rast.2013.6581267
https://doi.org/10.1109/rast.2013.6581267
Autor:
Caglar Ozyurt, Halime Urek, Emre Yurtoglu, Kurtulus Yilmaz, O. Tarakcioglu, M. Emin Gulluoglu, Deger Akin, Koray Celik, Aykut Kutlu, Emre Yavuzoglu, Erhan Topal, Kutlay Aydin
Publikováno v:
Proceedings of 5th International Conference on Recent Advances in Space Technologies - RAST2011.
Large torque amplification and momentum storage capacity are the two basic properties that make control moment gyroscopes (CMGs) superior when compared to the reaction and momentum wheels commonly used in spacecraft attitude control. Software and Har
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::291f1aba76b0ab36958b37f8f8754587
https://doi.org/10.1109/rast.2011.5966897
https://doi.org/10.1109/rast.2011.5966897