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

Aero-Thermo-Structural Trade-Off Studies for Hypersonic Transport Gliders based on the DLR SpaceLiner Concept

Kopp, Alexander (2015) Aero-Thermo-Structural Trade-Off Studies for Hypersonic Transport Gliders based on the DLR SpaceLiner Concept. In: AIAA 2015-3645. American Institute of Aeronautics and Astronautics. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference (Hypersonics 2015), 2015-07-06 - 2015-07-09, Glasgow, Scotland. doi: 10.2514/6.2015-3645.

[img] PDF
2MB

Offizielle URL: http://arc.aiaa.org/doi/abs/10.2514/6.2015-3645

Kurzfassung

The Space Launcher Systems Analysis Group SART of the German Aerospace Center DLR has been working for several years on developing a novel hypersonic passenger transportation concept. The SpaceLiner, originally proposed in 2005, is a two staged, rocket propelled and vertical take-off transportation system designed for a 90 minutes Europe-Australia reference mission carrying 50 passengers. The SpaceLiner has gone through several design cycles, with the most recent configuration SpaceLiner7-3 currently under definition. Various papers on the vehicle design as well as design of individual subsystems have been published over the years. One important finding was the high level of interdependency of the different technical disciplines and subsystems within a large design space, which on the one hand complicates the identification of optimum design solutions, while on the other hand offering unexpected performance increase potentials. Therefore, the work presented in this paper will leave the baseline configuration of the SpaceLiner and perform parametric system studies on a broader level. The aim is to identify and quantify interactions and interdependencies within the design space in order to provide design improvements for a potential future SpaceLiner configuration, as well as for vehicles of this class in general. Thereby, this work will investigate the design task on a pure parametric way due to the high complexity of the problem. An automated system analysis loop is utilized, but no multi-disciplinary optimization procedures will be applied. The parametric studies are still in progress, with first results being presented in this paper.

elib-URL des Eintrags:https://elib.dlr.de/102277/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Aero-Thermo-Structural Trade-Off Studies for Hypersonic Transport Gliders based on the DLR SpaceLiner Concept
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Kopp, Alexanderalexander.kopp (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:9 Juli 2015
Erschienen in:AIAA 2015-3645
Referierte Publikation:Ja
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
DOI:10.2514/6.2015-3645
Verlag:American Institute of Aeronautics and Astronautics
Status:veröffentlicht
Stichwörter:hypersonic passenger transportation, SpaceLiner, parametric system studies
Veranstaltungstitel:20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference (Hypersonics 2015)
Veranstaltungsort:Glasgow, Scotland
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:6 Juli 2015
Veranstaltungsende:9 Juli 2015
Veranstalter :AIAA
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 - Raumfahrzeugsysteme - Systemanalyse Raumtransport (alt)
Standort: Bremen
Institute & Einrichtungen:Institut für Raumfahrtsysteme
Hinterlegt von: Vormschlag, Nele Marei
Hinterlegt am:21 Jan 2016 09:33
Letzte Änderung:24 Apr 2024 20:08

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.