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Titel:

Polaris - Design of Liquid Hydrogen Turbo-Electric Transport Aircraft

Autor(en): T. Dietl, J. Karger, K. Kaupe, A. Pfemeter, P. Weber, A. Zakrzewski, A. Strohmayer
Zusammenfassung: Polaris is a liquid hydrogen turbo-electric transport aircraft which is designed to fulfill the NASA N 3 goals for entry into service in 2045. The main objective is to reduce the energy consumption by at least 60% compared to an A320 of 2005. Secondary objectives are the reduction of the NOX emissions by 80% and minimizing the noise emissions. The concept combines the synergies of a liquid hydrogen fuel system with a HTS power transmission and an intercooled gas turbine. By this a reduction of 62% in energy consumption and 80% lower NOx emissions are achieved at a comparable design mission.
Veranstaltung: Deutscher Luft- und Raumfahrtkongress 2018, Friedrichshafen
Verlag, Ort: Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2018
Medientyp: Conference Paper
Sprache: englisch
Format: 21,0 x 29,7 cm, 10 Seiten
URN: urn:nbn:de:101:1-2018122111550018979174
DOI:10.25967/480344
Stichworte zum Inhalt: Liquid Hydrogen, Turbo-electric, Hybrid-electric, Superconducting, Open-rotor, Transport aircraft
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Zitierform:Dietl, T.; Karger, J.; et al. (2018): Polaris - Design of Liquid Hydrogen Turbo-Electric Transport Aircraft. Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V.. (Text). https://doi.org/10.25967/480344. urn:nbn:de:101:1-2018122111550018979174.
Veröffentlicht am: 21.12.2018