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THOR - Innovative Thermal Management Concepts for Future Space Vehicles

Esser, Burkard (2016) THOR - Innovative Thermal Management Concepts for Future Space Vehicles. 8th European Workshop on Thermal Protection Systems and Hot Structures, 19.-22. April 2016, Noordwijk, Niederlande.

Full text not available from this repository.

Official URL: http://congrexprojects.com/custom/16c07/

Abstract

For future space vehicles significant improvements in flight performance are required in the long term. Next generation orbiters and to a huge extent hypersonic transport vehicles will need fast flight path control for efficient operation, a requirement that cannot be met with extremely blunted components. A significant reduction of bluntness, however, means significantly higher peak heat loads which are beyond the capabilities of the conventional thermal management concept. Future thermal management concepts will need to be defined globally. The main challenges for thermal management will be an equilibration of thermal loading by transferring heat efficiently from highly loaded surface areas to less loaded regions and the consideration and inclusion of active cooling techniques. Within the European FP7 research project THOR, four thermal management concepts were considered which all appeared well suited for global thermal management a priori. The concepts were defined based on recent progress in base material development, providing new materials with tailored properties for being integrated in thermal protection systems, as e.g. carbon-based fibres with a huge thermal conductivity which exceeds the conductivity of conventional fibres by at least an order of Magnitude, and SiC based ceramic foams with operational temperatures being very close to those of conventional dense ceramic matrix composite (CMC) materials. Experimentally, a significant potential had been observed and validated for the reduction of surface temperatures by the long-distance thermal exchange capabilities of thermal radiation and by transpiration cooling of external surfaces.

Item URL in elib:https://elib.dlr.de/105528/
Document Type:Conference or Workshop Item (Speech)
Title:THOR - Innovative Thermal Management Concepts for Future Space Vehicles
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Esser, BurkardBurkard.Esser (at) dlr.deUNSPECIFIED
Date:July 2016
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Atmospheric, Thermal Protection, Thermal Management, High Enthalpy Flow, Future Space Vehicles, Hypersonic Transport
Event Title:8th European Workshop on Thermal Protection Systems and Hot Structures
Event Location:Noordwijk, Niederlande
Event Type:international Conference
Event Dates:19.-22. April 2016
Organizer:ESA/ESTEC
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 - Raumfahrzeugsysteme - Rückkehrtechnologie
Location: Köln-Porz
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Über- und Hyperschalltechnologien
Deposited By: Esser, Dr.-Ing. Burkard
Deposited On:05 Sep 2016 09:09
Last Modified:05 Sep 2016 09:09

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