elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Impressum | Datenschutz | Kontakt | English
Schriftgröße: [-] Text [+]

The SHEFEX Flight Test and Development Program

Weihs, Hendrik (2013) The SHEFEX Flight Test and Development Program. 4th International ARA Days, 2013-05-27 - 2013-05-29, Arcachon, Frankreich.

[img] PDF
5MB

Kurzfassung

Within SHEFEX the step by step development results in stepwise increasing velocity and test duration. SHEFEX I performs a Mach 6 flight for 20 Seconds. SHEFEX II reaches Mach 10-11 for 45 Seconds. SHEFEX III is aimed to reach Mach 20 for 15 minutes, a significant and ambitious step which require a big sounding rocket which is currently not available, but under development in Brasil. Thus, the growing complexity of SHEFEX III is the right milestone within the Re-entry technology development road map to implement strategic co-operations and partnerships. On the test vehicle side, DLR leads the development with ASTRIUM as a strong industrial partner. On the launcher side, Brasil leads the VLM-1 Microlauncher development with DLR as a partner for the first application of the launch system within the SHEFEX III flight. But SHEFEX is not only a single path development for Re-entry. In the field of hypersonic aircraft and air breathing propulsion development the SHEFEX launch systems could be a standard rocket family for flight tests. The improvements in high temperature stable stabilizers, huge lift fairings to cover complex vehicles and high accurate pointing and control systems are applicable especially to such kinds of flight tests, which partially is already done within the HiFire and Scramspace Programs and could be used within the ESA HEXAFLY proposal. This paper will give an overview of the running SHEFEX III project and the related REX Free Flyer study. Also some related Spin off activities will be discussed

elib-URL des Eintrags:https://elib.dlr.de/87595/
Dokumentart:Konferenzbeitrag (Vortrag)
Zusätzliche Informationen:Eingeladener Plenarvortrag
Titel:The SHEFEX Flight Test and Development Program
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Weihs, HendrikBK-RSINICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:Mai 2013
Referierte Publikation:Nein
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:SHEFEX, Wiedereintritt, Flugexperiment, Hyperschall
Veranstaltungstitel:4th International ARA Days
Veranstaltungsort:Arcachon, Frankreich
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:27 Mai 2013
Veranstaltungsende:29 Mai 2013
Veranstalter :The Atmospheric Reentry Association
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Raumtransport
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R RP - Raumtransport
DLR - Teilgebiet (Projekt, Vorhaben):R - SHEFEX Programm (alt)
Standort: Stuttgart
Institute & Einrichtungen:Institut für Bauweisen- und Konstruktionsforschung > Raumfahrt- System- Integration
Hinterlegt von: Weihs, Hendrik
Hinterlegt am:14 Jan 2014 08:49
Letzte Änderung:24 Apr 2024 19:53

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

Blättern
Suchen
Hilfe & Kontakt
Informationen
electronic library verwendet EPrints 3.3.12
Gestaltung Webseite und Datenbank: Copyright © Deutsches Zentrum für Luft- und Raumfahrt (DLR). Alle Rechte vorbehalten.