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The sharp edge flight experiment SHEFEX

Weihs, H. and Longo, J. and Gülhan, A. (2002) The sharp edge flight experiment SHEFEX. 4th European Workshop on Hot Structures and TPS for Space Vehicles, Palermo, Italien, 26-29 November 2002.

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Abstract

This paper describes a currently running basic research project of the German Aerospace Center (DLR). The aim is to investigate the behaviour and possibilities of a new shape for re-entry vehicles considering sharp edges and facetted surfaces. The SHEFEX vehicle is a kind of flying wind tunnel test object. The aim is to correlate numerical analysis, wind tunnel test results and real flight data in terms of aerodynamic effects and structural concept for the thermal protection system.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2003,
Title:The sharp edge flight experiment SHEFEX
Authors:
AuthorsInstitution or Email of Authors
Weihs, H.UNSPECIFIED
Longo, J.AT-BS
Gülhan, A.AT-KP
Date:2002
Status:Published
Keywords:ceramic matrix composites, hot structures, re-entry
Event Title:4th European Workshop on Hot Structures and TPS for Space Vehicles, Palermo, Italien, 26-29 November 2002
Organizer:ESA/ASI/DLR/CNES
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):UNSPECIFIED
Location: Stuttgart
Institutes and Institutions:Institute of Structures and Design
Deposited By: elib DLR-Beauftragter
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 22:32

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