Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Hendrik Weihs"'
Publikováno v:
International Journal of Aerospace Engineering, Vol 2019 (2019)
The second sharp-edged flight experiment is a faceted suborbital reentry body that enables low-cost in-flight reentry research. Its faceted thermal protection system consisting of only flat radiation-cooled thermal protection panels is cost-efficient
Externí odkaz:
https://doaj.org/article/75ea699164fe451395d545443dc47ab5
Publikováno v:
International Journal of Aerospace Engineering, Vol 2019 (2019)
The second sharp-edged flight experiment is a faceted suborbital reentry body that enables low-cost in-flight reentry research. Its faceted thermal protection system consisting of only flat radiation-cooled thermal protection panels is cost-efficient
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3dbe98c571f70c74b534721143d15787
https://doi.org/10.1155/2019/9754739
https://doi.org/10.1155/2019/9754739
The design of a reentry vehicle strongly depends on the entry strategy of the projected mission. From the aerodynamic point of view, the layout of a hypersonic vehicle is a compromise between a veh...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4d699138a5dbe8cdd58bb914ac1b92e6
https://doi.org/10.2514/1.a33965
https://doi.org/10.2514/1.a33965
The octahedral sharp leading edge of the sharp edge flight experiment SHEFEX II is made from carbon fiber reinforced ceramic with a tip radius of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::69ab654a7f1b7135a623547d3af88195
https://elib.dlr.de/91996/
https://elib.dlr.de/91996/
Publikováno v:
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference.
The octahedral sharp leading edge of SHEFEXII is made from C/C-SiC fiber reinforced ceramic. It is instrumented by three thermocouples and eight pressure ports. A duplicate was ground-tested in arc-heated wind tunnel L3K. Transient thermal response o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3eae9b4eaf11b0e9b197e19cd05d1b15
https://doi.org/10.2514/6.2012-5919
https://doi.org/10.2514/6.2012-5919
Publikováno v:
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference.
The German Aerospace Center (DLR) has developed a ceramic fin experiment (FinEx) for the HIFiRE-5 flight in order to test the performance of new structures with sharp leading edges during flight. The analysis of the thermal performance of the fin has
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::63fc647992fd61c8b870d5e2fba93b49
https://doi.org/10.2514/6.2012-5920
https://doi.org/10.2514/6.2012-5920
Publikováno v:
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7d1dd8433b1d5d219babb7d3ab3ce974
https://doi.org/10.2514/6.2009-7426
https://doi.org/10.2514/6.2009-7426
After the successful flight of SHEFEX I the next mission is under development. Within this paper the basic goals and architecture of the SHEFEX II mission will be presented. Also launched by a two staged sounding rocket system SHEFEX II will be a con
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::fe50831050fff188d1bf8d1ec2463fc0
https://elib.dlr.de/56131/
https://elib.dlr.de/56131/
Autor:
Thino Eggers, Hendrik Weihs, Marcus Hörschgen, Günther Requardt, Frank Siebe, Wolfgang Jung, Torsten Laux, Thomas Reimer, Ali Gülhan, Andreas Stamminger, John Turner, Jose M. A. Longo
On Thursday, October 27th, 2005 the SHarp Edge Flight EXperiment SHEFEX has been successfully launched at the Andoya Rocket Range in northern Norway. The project, being performed under responsibility of the German Aerospace Center (DLR) flew on top o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::84b5943b17e6af1fe6dd64b338d9be63
https://elib.dlr.de/47421/
https://elib.dlr.de/47421/