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High Enthalpy Testing of UHTCMC Materials for Space Application

Esser, Burkard and Gülhan, Ali and Reimer, Thomas (2019) High Enthalpy Testing of UHTCMC Materials for Space Application. Int. Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions & Engineering, 30. Sept. - 3. Okt. 2019, Monopoli, Italien.

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Abstract

The European Union H2020 project C3HARME has been established for investigations on fibre reinforced ultra-high temperature ceramics with regard to their detailed mechanical and thermal characterization and further qualification for application in harsh propulsion and space environments. This paper is focusing on the qualification of these materials for use as a surface layer of a thermal protection system for atmospheric entry. Test requirements, the test facility, details of experimental setup and test conditions are being discussed in particular.

Item URL in elib:https://elib.dlr.de/134013/
Document Type:Conference or Workshop Item (Speech)
Title:High Enthalpy Testing of UHTCMC Materials for Space Application
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Esser, BurkardBurkard.Esser (at) dlr.deUNSPECIFIED
Gülhan, AliAli.Guelhan (at) dlr.deUNSPECIFIED
Reimer, ThomasThomas.Reimer (at) dlr.deUNSPECIFIED
Date:2019
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Thermal protection, arc-heated facility, high enthalpy testing, ultra-high temperature ceramics
Event Title:Int. Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions & Engineering
Event Location:Monopoli, Italien
Event Type:international Conference
Event Dates:30. Sept. - 3. Okt. 2019
Organizer:ESA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Wiederverwendbare Raumfahrtsysteme
Location: Köln-Porz , Stuttgart
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Supersonoc and Hypersonic Technology
Institute of Structures and Design > Space System Integration
Deposited By: Esser, Dr.-Ing. Burkard
Deposited On:12 Feb 2020 07:39
Last Modified:12 Feb 2020 07:41

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