Schwanekamp, Tobias und Meyer, Frank und Reimer, Thomas und Petkov, Ivaylo und Tröltzsch, Anke und Siggel, Martin (2014) System Studies on Active Thermal Protection of a Hypersonic Suborbital Passenger Transport Vehicle. In: AIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2014. AIAA. 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2014-06-16 - 2014-06-20, Atlanta, GA, USA. doi: 10.2514/6.2014-2372.
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Kurzfassung
Aerodynamic heating is a critical design aspect for the development of reusable hypersonic transport and reentry vehicles. The reliability in terms of thermal resistance is one of the major driving factors with respect to the design margins, the mass balance and finally the total costs of a configuration. Potential designs of active cooling systems for critical regions such as the vehicle nose and leading edges are presented as well as preliminary approaches for their impact on the total mass. The visionary suborbital passenger transport concept SpaceLiner is taken as a reference vehicle for these studies. Covering the whole flight regime from subsonic to Mach numbers of more than 20, this vehicle creates high demands on the thermal protection system. Part of the work was performed within the DLR research project THERMAS.
elib-URL des Eintrags: | https://elib.dlr.de/92953/ | ||||||||||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||||||
Titel: | System Studies on Active Thermal Protection of a Hypersonic Suborbital Passenger Transport Vehicle | ||||||||||||||||||||||||||||
Autoren: |
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Datum: | Juni 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: | 10.2514/6.2014-2372 | ||||||||||||||||||||||||||||
Herausgeber: |
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Verlag: | AIAA | ||||||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||||||
Stichwörter: | Thermal Protection System, Active Cooling, Hypersonic Passenger Transport, Aerodynamic Heating, SpaceLiner | ||||||||||||||||||||||||||||
Veranstaltungstitel: | 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference | ||||||||||||||||||||||||||||
Veranstaltungsort: | Atlanta, GA, USA | ||||||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||||||
Veranstaltungsbeginn: | 16 Juni 2014 | ||||||||||||||||||||||||||||
Veranstaltungsende: | 20 Juni 2014 | ||||||||||||||||||||||||||||
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), R - Proj. Thermas (alt) | ||||||||||||||||||||||||||||
Standort: | Stuttgart | ||||||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Raumfahrtsysteme > Systemanalyse Raumtransport Institut für Bauweisen und Strukturtechnologie Institut für Simulations- und Softwaretechnik Institut für Simulations- und Softwaretechnik > Verteilte Systeme und Komponentensoftware | ||||||||||||||||||||||||||||
Hinterlegt von: | Schwanekamp, Tobias | ||||||||||||||||||||||||||||
Hinterlegt am: | 09 Dez 2014 14:27 | ||||||||||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 19:58 |
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