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pro vyhledávání: '"SHEFEX"'
Akademický článek
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Publikováno v:
Journal of Spacecraft and Rockets. 53:153-177
The aerothermal instrumentation of the Sharp Edge Hypersonic Flight Experiment SHEFEX-II, which was launched from Andoya Rocket Range on top of a two-stage rocket configuration, provided very useful flight data. Complementary to the pressure data, he
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::19a4c7aa66b1b978997711886a10b738
https://doi.org/10.2514/1.a33275
https://doi.org/10.2514/1.a33275
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
Autor:
Hannah Böhrk
Publikováno v:
Journal of Spacecraft and Rockets. 52:674-683
The present paper presents the in-flight measurement of the transpiration cooling experiment Aktive Kuhlung durch Transpiration im Versuch (often referred to as AKTiV) flown on the suborbital reentry configuration Sharp Edge Flight Experiment II (oft
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::01be40ee6dbf4306ffd2b294cd1631a4
https://doi.org/10.2514/1.a33144
https://doi.org/10.2514/1.a33144
Autor:
Franze, Marius
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
This work is subsequent to the aerodynamic and atmospheric analysis presented in an earlier paper, which presumed a structural deformation of the main fins of SHEFEX II. For this reason the ascend phase of the vehicle is analyzed to get the maximum s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::893e5a5e1d95d11806aad85ce0f72034
https://doi.org/10.2514/6.2016-3237
https://doi.org/10.2514/6.2016-3237
Autor:
Marius Franze
Numerical predictions by coupling the aerodynamic code DLR TAU with trajectory optimization program REENT-6D for different atmospheric models are presented in this paper. Using balloon data and existing models, an atmospheric model has been developed
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::406c7115afba5beb5dc74d89c815ea46
https://elib.dlr.de/103179/
https://elib.dlr.de/103179/