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pro vyhledávání: '"SHEFEX II"'
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Autor:
Sven Lorenz, Andreas Bierig
Publikováno v:
AIAA Guidance, Navigation, and Control (GNC) Conference.
This paper presents the simulation based robustness analysis w.r.t. parameters and initial conditions, related to the hypersonic flight experiment called SHEFEX-II. The robustness criteria and the parameter limits are obtained from the nominal missio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b09f8f3dc61fbaecc96f3e453f30fc41
https://doi.org/10.2514/6.2013-4857
https://doi.org/10.2514/6.2013-4857
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/
Autor:
Ettl, Josef, Turner, John
The SHEFEX II sounding rocket vehicle comprised a two stage VS40 motor combination, whereby the first stage was passively aerodynamically stabilized by canted fins but the spinning second stage motor and payload, was repointed before ignition and con
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1640::a8b498cb13eff40f35d71c7bcf8f6cab
https://elib.dlr.de/89241/
https://elib.dlr.de/89241/
Autor:
Hannah Böhrk
Publikováno v:
11th AIAA/ASME Joint Thermophysics and Heat Transfer Conference.
The present paper presents the in-flight measurement of the transpiration cooling experiment AKTiV flown on the sub-orbital re-entry configuration SHEFEXII. Thermal response of the structure is measured just up- and downstream of a cooled sample with
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d07bd878611d6248918d4c9753b3b8e9
https://doi.org/10.2514/6.2014-2676
https://doi.org/10.2514/6.2014-2676