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Potential Propulsion Architecture for a Reduced Climate Impact of Civil Aviation

Atanasov, Georgi (2020) Potential Propulsion Architecture for a Reduced Climate Impact of Civil Aviation. E2FLIGHT Conference 2020, 2020-02-20 - 2020-02-21, Stuttgart, Deutschland. (Unpublished)

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Abstract

The presentation focuses on the assessment of a hybrid-electric propulsion architecture with a battery as the main power provider for reduced emissions on short distances and kerosene driven range extender for range flexibility and for mission reserves, in the context of global environmental impact of aviation.

Item URL in elib:https://elib.dlr.de/140053/
Document Type:Conference or Workshop Item (Speech)
Title:Potential Propulsion Architecture for a Reduced Climate Impact of Civil Aviation
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Atanasov, GeorgiUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:21 February 2020
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:Battery, Electric, Aircraft, Emissions
Event Title:E2FLIGHT Conference 2020
Event Location:Stuttgart, Deutschland
Event Type:Other
Event Start Date:20 February 2020
Event End Date:21 February 2020
Organizer:DLR
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Concepts and Integration (old)
Location: Hamburg
Institutes and Institutions:Institute of System Architectures in Aeronautics > Aircraft Design and System Integration
Deposited By: Atanasov, Georgi
Deposited On:11 Jan 2021 08:25
Last Modified:24 Apr 2024 20:41

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