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SHEFEX - Hypersonic Re-entry Fllight Experiment - Vehicle and Subsystem Design, Flight Performance and Prospects

Turner, John and Hörschgen, Marcus and Jung, Wolfgang and Stamminger, Andreas and Turner, Peter (2006) SHEFEX - Hypersonic Re-entry Fllight Experiment - Vehicle and Subsystem Design, Flight Performance and Prospects. In: Proceedings AIAA 14th Spaceplane Systems and Technologies Conference. 14th Spaceplane Systems and Technologies Conference, 2006-11-08, Canberra, Australia.

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Abstract

The purpose of the Sharp Edge Flight Experiment (SHEFEX) was to investigate the aerodynamic behavior and thermal problems of an unconventional shape for re-entry vehicles comprising multi-facetted surfaces with sharp edges. The main object of this experiment was the correlation of numerical analysis with real flight data with respect to the aerodynamic effects and structural concept for the thermal protection system (TPS). The Mobile Rocket Base of the German Aerospace Center (DLR) was responsible for the test flight of SHEFEX on a two-stage unguided solid propellant sounding rocket, which was required to provide a velocity of the order of Mach 7. The SHEFEX vehicle was launched on the 27th of October 2005 from the Andoya Rocket Range, Norway. This paper presents the main design features of the vehicle and subsystems, the flight performance and the current plans for our next hypersonic project.

Item URL in elib:https://elib.dlr.de/48073/
Document Type:Conference or Workshop Item (Speech)
Title:SHEFEX - Hypersonic Re-entry Fllight Experiment - Vehicle and Subsystem Design, Flight Performance and Prospects
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Turner, JohnTwIGUNSPECIFIED
Hörschgen, MarcusUNSPECIFIEDUNSPECIFIED
Jung, WolfgangUNSPECIFIEDUNSPECIFIED
Stamminger, AndreasUNSPECIFIEDUNSPECIFIED
Turner, PeterUNSPECIFIEDUNSPECIFIED
Date:8 November 2006
Journal or Publication Title:Proceedings AIAA 14th Spaceplane Systems and Technologies Conference
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmail
AIAA, UNSPECIFIED
Status:Published
Keywords:SHEFEX, Wiedereintritt, Höhenforschungsrakete, Hyperschall, Flugexperiment, SHEFEX, Reentry, Sounding Rocket, Hypersonic, Flight Experiment
Event Title:14th Spaceplane Systems and Technologies Conference
Event Location:Canberra, Australia
Event Type:international Conference
Event Dates:2006-11-08
Organizer:AIAA
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: Oberpfaffenhofen
Institutes and Institutions: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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