Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Erhan Serbest"'
Publikováno v:
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
The current qualification status of the Ariane 5 SCA - Systeme Controle d'Attitude - 400 N monopropellant hydrazine thruster developed on ESA funding under CNES responsibility is presented. The qualification status is mainly based on several qualific
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::201abaa3e022541f6a81ac49b4b5893b
https://doi.org/10.2514/6.2003-4779
https://doi.org/10.2514/6.2003-4779
Publikováno v:
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7715d6b29c9b7ad0a0b435c6d95300d0
https://doi.org/10.2514/6.2002-4157
https://doi.org/10.2514/6.2002-4157
Publikováno v:
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f7ff7bc0bd3cd79a8189f9609b2f8da7
https://doi.org/10.2514/6.2002-4283
https://doi.org/10.2514/6.2002-4283
Publikováno v:
37th Joint Propulsion Conference and Exhibit.
This report summarizes the experimental work in the field of effusion cooling done with C/C (carbon fibres in carbon matrix) for a porous cylinder in combination with a porous nozle. The experiments presented here have been realized using gaseous hyd
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::29cb84435569896f8eed01a583c8c88a
https://doi.org/10.2514/6.2001-3410
https://doi.org/10.2514/6.2001-3410
Blowing through the wall is one of the most efficient methods to influence the characteristics of a turbulent boundary layer such as heat transfer, skin friction, boundary-layer profiles, and flow separation. The most important technical application
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::fc14ddf3fbda9c7427c2858b905c5cc4
https://elib.dlr.de/1545/
https://elib.dlr.de/1545/
Publikováno v:
34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Introduction While previous experimental activities of DLR focused on low pressure applications of combustion chamber segments cooled with either water or gaseous hydrogen wich have been performed at the DLR test facilities P6.1 and M3, this paper pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::46085c22b8d12abad80e8afd39b447f1
https://doi.org/10.2514/6.1998-3443
https://doi.org/10.2514/6.1998-3443