Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Ahmet Bilge Uygur"'
Autor:
Ahmet Bilge Uygur
Publikováno v:
Havacılık ve Uzay Teknolojileri Dergisi, Vol 11, Iss 1, Pp 17-27 (2018)
This paper describes a complete methodology for the computation of transient external heat fluxes (i.e. solar, albedo and earth) for a given set of orbital parameters such as altitude, solar constant etc. and orientation of the satellite. A software
Externí odkaz:
https://doaj.org/article/b482330aa06a49c7b3541e268c287d7c
Publikováno v:
Havacılık ve Uzay Teknolojileri Dergisi, Vol 9, Iss 1, Pp 57-64 (2016)
This paper focuses on a practical, low budget image processing approach developed to quantify the damping effect on moment of inertia measurements performed withan inverted torsional pendulum. Several measurement cases were realized to measure the da
Externí odkaz:
https://doaj.org/article/0bafa048a80347bd86bd4dcb05c85b48
Publikováno v:
International Journal of Pressure Vessels and Piping. 165:241-248
In this study, a reliable and novel testing methodology is presented for the burst test of heat pipes developed for space applications. The test set up enables heat pipe to be tested at flight configuration. The target internal pressure of the heat p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::adb862ccec225cbb499538d768166990
https://doi.org/10.1016/j.ijpvp.2018.07.002
https://doi.org/10.1016/j.ijpvp.2018.07.002
Publikováno v:
2015 7th International Conference on Recent Advances in Space Technologies (RAST).
In this paper, the new Space Systems Assembly, Integration and Test (AIT) center established within Turkish Aerospace Industries, Inc (TAI) premises in Ankara will be described. The AIT capabilities of the center will be explained. Key specifications
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5f9924089559a3ccde66fb05c3e2c598
https://doi.org/10.1109/rast.2015.7208318
https://doi.org/10.1109/rast.2015.7208318
Publikováno v:
2015 7th International Conference on Recent Advances in Space Technologies (RAST).
Satellites are exposed to simultaneous static and dynamic loads during the launch phase due to launcher acceleration and aerodynamics. Therefore, they are designed and tested to withstand all these loads. From design perspective, a common approach is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::120194de41f1d2414a1fbcb3efbc182d
https://doi.org/10.1109/rast.2015.7208381
https://doi.org/10.1109/rast.2015.7208381
Publikováno v:
2009 4th International Conference on Recent Advances in Space Technologies.
This paper discusses the development of an in-house computer code for the thermal analysis of satellites. The code uses Thermal Network Method (TNM) in conjunction with the Method of Lines (MOL) for the solution of the energy equation in the presence
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6609f382b1210b867d6a312103269768
https://doi.org/10.1109/rast.2009.5158247
https://doi.org/10.1109/rast.2009.5158247