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High Enthalpy Testing of UHTC Materials for Space Application

Esser, Burkard und Gülhan, Ali (2017) High Enthalpy Testing of UHTC Materials for Space Application. Ultra-High Temperature Ceramics: Materials for Extreme Environment Applications IV, 2017-09-17 - 2017-09-20, Windsor, Großbritannien. (nicht veröffentlicht)

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Kurzfassung

Space vehicles are subjected to severe heat loads when entering a planetary atmosphere and require a powerful thermal protection system (TPS). The protection systems' thermal efficiency can strongly be enhanced by using surface materials with substantial radiative cooling capabilities, which are directly correlated to high operational temperatures. Accordingly, ablative and UHTC materials are well-suited for use in TPS structures. Due to their physical integrity, UHTC materials are an appropriate choice for future reusable space vehicles, which are requiring improved thermal efficiencies compared with state-of-the-art systems, resulting from demands on enhanced flight performance parameters. Advanced stages of material development include experimental characterization and qualification at realistic environmental conditions. Arc-heated facilities, as e.g. DLR's arc heated facilities LBK with its two test legs L2K and L3K, are well suited for testing materials for thermal protection issues, since they allow for testing at realistic convective and catalytic heat fluxes. During the last decades, several test conditions have been established in L2K and L3K and were applied to both, ablative and UHTC materials. Heat fluxes range up to more than 10 MW/m2. In the frame the European project ABLAMOD and the ESA funded CHEF study, selected test conditions were further characterized by sophisticated spectroscopic measurement techniques. These measurements confirmed the common assumption that the reservoir conditions can be considered in thermal equilibrium.

elib-URL des Eintrags:https://elib.dlr.de/118218/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:High Enthalpy Testing of UHTC Materials for Space Application
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Esser, BurkardBurkard.Esser (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Gülhan, AliAli.Guelhan (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:2017
Referierte Publikation:Nein
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:nicht veröffentlicht
Stichwörter:High enthalpy testing, thermal protection, material characterization and qualification, future space vehicles
Veranstaltungstitel:Ultra-High Temperature Ceramics: Materials for Extreme Environment Applications IV
Veranstaltungsort:Windsor, Großbritannien
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:17 September 2017
Veranstaltungsende:20 September 2017
Veranstalter :Engineering Conferences International
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 - Wiederverwendbare Raumfahrtsysteme (alt)
Standort: Köln-Porz
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik > Über- und Hyperschalltechnologien, KP
Hinterlegt von: Esser, Dr.-Ing. Burkard
Hinterlegt am:07 Jun 2018 09:26
Letzte Änderung:24 Apr 2024 20:22

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