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Investigation of Structure, Thermal Protection System, and Passenger Stage Integration for the Hypersonic Transport System SpaceLiner

Kopp, Alexander und Garbers, Nicole (2014) Investigation of Structure, Thermal Protection System, and Passenger Stage Integration for the Hypersonic Transport System SpaceLiner. In: AIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2014. 14th AIAA Aviation Technology, Integration, and Operations Conference, 2014-06-16 - 2014-06-20, Atlanta. doi: 10.2514/6.2014-2531.

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Kurzfassung

Suborbital high speed transport is a technology that could significantly impact space transportation, since mass production of rocket propelled aircraft and their engines, as well as operating them on a routinely basis, promises reductions in the manufacturing and launching costs for space launchers. With this vision in mind, the SpaceLiner concept was developed in the Space Launcher Systems Analysis group (SART) of DLR in 2005. Since then, the original design has evolved into several successive configurations. The latest configuration 7-2 is shown in Fig. 1. Currently, the configuration 7-3 is under definition. Various papers have been published about the SpaceLiner or its subsystems, for instance Ref. 1 and Ref. 2 as some of the latest ones. The SpaceLiner is a two staged, rocket propelled and vertical lift off passenger transport aircraft. The reference mission is to carry 50 passengers from Europe to Australia or vice versa within just 90 minutes. The SpaceLiner system is composed of a winged, passenger carrying main stage also denominated orbiter, and a winged booster. Both stages are liquid oxygen (LOX) and liquid hydrogen (LH2) propelled, and fully reusable. After booster separation, the orbiter continues the ascent with its own rocket engines until main engine cut-off (MECO) at an altitude of around 75 km. Subsequently, the range flight is being performed in gliding mode, whereas Mach numbers of up to 24 are reached.

elib-URL des Eintrags:https://elib.dlr.de/91274/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Investigation of Structure, Thermal Protection System, and Passenger Stage Integration for the Hypersonic Transport System SpaceLiner
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Kopp, Alexanderalexander.kopp (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Garbers, Nicolenicole.garbers (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:2014
Erschienen in:AIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2014
Referierte Publikation:Nein
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Nein
DOI:10.2514/6.2014-2531
Status:veröffentlicht
Stichwörter:Thermal Protection System, Passenger Stage Integration, Hypersonic Transport System, SpaceLiner
Veranstaltungstitel:14th AIAA Aviation Technology, Integration, and Operations Conference
Veranstaltungsort:Atlanta
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:16 Juni 2014
Veranstaltungsende:20 Juni 2014
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 > Systemanalyse Raumtransport
Hinterlegt von: Behnke, Manuela
Hinterlegt am:12 Feb 2015 09:42
Letzte Änderung:24 Apr 2024 19:57

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