Böhrk, Hannah und Thiele , Thomas und Dittert, Christian und Weihs, Hendrik und Gülhan, Ali (2012) Thermal Testing of the Sharp Leading Edge of SHEFEXII. 18th International Space Planes and Hypersonic Systems and Technologies Conference, 2012-09-24 - 2012-09-28, Tours, Frankreich.
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Kurzfassung
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 of the material to the load was also determined by the heat-balance method HEATS and compared to the measurement data. During ground-testing, the hermocouples measured 1179°C, whereas the maximum temperature recorded during flight was measured at 30km altitude with 848°C. The simulated data corresponds well to both thermocouple data and data from an external infrared camera. During ground-testing, the very tip of the leading edge reaches 1635°C. The nose was in good order after ground testing.
elib-URL des Eintrags: | https://elib.dlr.de/77663/ | ||||||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag, Paper) | ||||||||||||||||||||||||
Titel: | Thermal Testing of the Sharp Leading Edge of SHEFEXII | ||||||||||||||||||||||||
Autoren: |
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Datum: | September 2012 | ||||||||||||||||||||||||
Referierte Publikation: | Nein | ||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||
Stichwörter: | Sharp Leading Edge, SHEFEX, thermal protection system, TPS | ||||||||||||||||||||||||
Veranstaltungstitel: | 18th International Space Planes and Hypersonic Systems and Technologies Conference | ||||||||||||||||||||||||
Veranstaltungsort: | Tours, Frankreich | ||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||
Veranstaltungsbeginn: | 24 September 2012 | ||||||||||||||||||||||||
Veranstaltungsende: | 28 September 2012 | ||||||||||||||||||||||||
Veranstalter : | AIAA/3AF | ||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||
HGF - Programm: | Raumfahrt | ||||||||||||||||||||||||
HGF - Programmthema: | Raumtransport | ||||||||||||||||||||||||
DLR - Schwerpunkt: | Raumfahrt | ||||||||||||||||||||||||
DLR - Forschungsgebiet: | R RP - Raumtransport | ||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | R - SHEFEX Programm (alt) | ||||||||||||||||||||||||
Standort: | Köln-Porz , Stuttgart | ||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Über- und Hyperschalltechnologien Institut für Bauweisen- und Konstruktionsforschung > Raumfahrt- System- Integration | ||||||||||||||||||||||||
Hinterlegt von: | Böhrk, Hannah | ||||||||||||||||||||||||
Hinterlegt am: | 16 Okt 2012 12:26 | ||||||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 19:43 |
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