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The Hypersonic Experiment SHEFEX - Aerotheromdynamic Layout, Vehicle Development and First Flight Results

Eggers, Thino and Stamminger, Andreas and Hörschgen, Marcus and Jung, Wolfgang and Turner, John (2005) The Hypersonic Experiment SHEFEX - Aerotheromdynamic Layout, Vehicle Development and First Flight Results. In: Proceedings 6th International Launcher Symposium on Launcher Technologies. 6th International Symposium on Launcher Technologies, 2005-11-08 - 2005-11-11, München, Deutschland.

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Abstract

The purpose of the SHarp Edge Flight Experiment SHEFEX was the investigation of the aerodynamic behaviour and thermal problems of possible new shapes for future launcher or re-entry vehicles. The main focus was the improvement of common space vehicle shapes by application of facetted surfaces and sharp edges. The experiment has permitted the accurate investigation of the flow effects and their structural solution during the hypersonic flight from 90 km down to an altitude of 20 km. The project, performed under responsibility of the German Aerospace Centre (DLR) was launched from Andoya Rocket Range, Norway on October 27th 2005. This paper introduces the mission, describes the layout of the experiment and the re-entry vehicle, as well as the development process of the complete flight vehicle and initial post flight results.

Item URL in elib:https://elib.dlr.de/48067/
Document Type:Conference or Workshop Item (Speech)
Title:The Hypersonic Experiment SHEFEX - Aerotheromdynamic Layout, Vehicle Development and First Flight Results
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Eggers, ThinoDLRUNSPECIFIED
Stamminger, AndreasDLRUNSPECIFIED
Hörschgen, MarcusDLRUNSPECIFIED
Jung, WolfgangDLRUNSPECIFIED
Turner, JohnTwIGUNSPECIFIED
Date:8 November 2005
Journal or Publication Title:Proceedings 6th International Launcher Symposium on Launcher Technologies
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Wiedereintritt, Höhenforschungsraketen, CFD, Hyperschall, SHEFEX, SHEFEX, Reentry, Sounding Rockets, CFD, Hypersonic
Event Title:6th International Symposium on Launcher Technologies
Event Location:München, Deutschland
Event Type:international Conference
Event Dates:2005-11-08 - 2005-11-11
Organizer:Onera
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):W - Vorhaben SHEFEX (old)
Location: Braunschweig , Oberpfaffenhofen , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Space Operations and Astronaut Training > MORABA-Mobile Rocket Base
Deposited By: Stamminger, Dr. Andreas
Deposited On:07 May 2007
Last Modified:31 Jul 2019 19:19

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