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Aerodynamic Analysis of the DLR Flight Experiment SHEFEX

Eggers, Th. und Barth, T. (2006) Aerodynamic Analysis of the DLR Flight Experiment SHEFEX. In: 14th Int. Space Planes and Hypersonic Systems and Technologies Conference. 14th Int. Space Planes and Hypersonic Systems and Technologies Conference, 2006-11-08, Canberra (Australia).

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Kurzfassung

On Thursday, October 27th, 2005 the SHarp Edge Flight EXperiment SHEFEX was successfully launched at the Andøya Rocket Range in northern Norway. The project, being performed under responsibility of the German Aerospace Center (DLR) flew on top of a two-stage solid propellant sounding rocket. One purpose of the experiment was the investigation of possible new shapes for future launcher or re-entry vehicles applying a shape with facetted surfaces and sharp edges and to enable the time accurate investigation of the flow effects and their structural answer during the hypersonic flight from 90 km down to an altitude of 20 km. During the flight surface pressures, temperatures and heat fluxes were measured and stored. Additionally, the output of the flown inertial platform provides the complete flight mechanic description (flight angles, accelerations, velocity and positions) from lift-off until the deployment of the recovery system. The present paper discusses the actual status of the aerodynamic analysis.

Dokumentart:Konferenzbeitrag (Vortrag, Paper)
Titel:Aerodynamic Analysis of the DLR Flight Experiment SHEFEX
Autoren:
AutorenInstitution oder E-Mail-Adresse der Autoren
Eggers, Th.NICHT SPEZIFIZIERT
Barth, T.NICHT SPEZIFIZIERT
Datum:November 2006
Erschienen in:14th Int. Space Planes and Hypersonic Systems and Technologies Conference
Referierte Publikation:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:SHEFEX, hypersonic, flight experiment, aerodynamics, post flight analysis
Veranstaltungstitel:14th Int. Space Planes and Hypersonic Systems and Technologies Conference
Veranstaltungsort:Canberra (Australia)
Veranstaltungsart:internationale Konferenz
Veranstaltungsdatum:2006-11-08
Veranstalter :AIAA
HGF - Forschungsbereich:Verkehr und Weltraum (alt)
HGF - Programm:Weltraum (alt)
HGF - Programmthema:W RP - Raumtransport
DLR - Schwerpunkt:Weltraum
DLR - Forschungsgebiet:W RP - Raumtransport
DLR - Teilgebiet (Projekt, Vorhaben):W - Vorhaben SHEFEX (alt)
Standort: Braunschweig
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik > Raumfahrzeuge
Hinterlegt von: Dr.-Ing. Thino Eggers
Hinterlegt am:07 Jun 2007
Letzte Änderung:12 Dez 2013 20:24

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