Preliminary Design of a 6-Seater Electric Aircraft
Abstract
A more sustainable and eco-friendly aircraft is needed for the near future, but current electric aircraft technology (e.g., electric motors and batteries) is still lacking compared to its fossil-fuel- based counterparts. To support the effort for fully electric aircraft maturity, an electric aircraft up to its preliminary design stage is developed using various analytical and software-based analyses with the target of fulfilling a set of design requirements and objectives for a 5000 kg MTOW 6-seater fully electric aircraft. The results of the aircraft preliminary design yield that overall, the aircraft fulfills all the requirements and most of the objectives. The design itself can still be further developed through optimization, re-evaluation, future studies, and upcoming technologies.
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E. A. E. Rodas, J. Lewe, D. N. Mavris, Feasibility Focused Design of Electric On-demands Aircraft Concepts, 2014.
S. Gudmundsson, General Aviation Aircraft Design: Applied Methods and Procedures, 1st ed.; ELSEVIER: Oxford, UK, 2014.
J. Roskam, Part I: Preliminary Sizing of Airplanes, DARcorporation: Kansas, USA, 1990.
D.P Raymer, Aircraft Design: A Conceptual Approach, 6th ed.; AAIA: Blacksburg, Virginia, 2018.
Jux B, Foitzik S, and Doppelbauer M 2018 A Standard Mission Profile for Hybrid-Electric Regional Aircraft based on Web Flight Data (Karlsruhe: Inst. Of Electrical Engineering).
M. H. Sadraey, Aircraft Design: A System Engineering Approach, 1st ed.; John Wiley & Sons Ltd: West Sussex, UK, 2013.
Prof. Dr. Hari Muhammad, Dr. Yazdi I Jenie l, AE3220 Flight Dynamics, Faculty of Mechanical and Aerospace Engineering ITB: Bandung, 2021.
E. Torenbeek, Synthesis of Subsonic Airplane Design; Delft University Press: Delft, Netherlands, 1982.
Ruijgrok G.J.J, Elements of Airplane Performance, 2nd ed.; VSSD: Delft, Netherlands, 2009.
.J. Roskam, Part VIII: Airplane Cost Estimation: Design, Development, Manufacturing and Operating, DARcorporation: Kansas, USA, 1990.
J. Roskam, Part III: Layout Design of Cockpit, Fuselage, Wing, and Empennage: Cutaways and Inboard Profiles, Kansas: Design, Analysis, and Research Corporation, 2002.
J. Roskam, Part II: Preliminary Configuration Design and Integration of the Propulsion System, Lawrence: DARcorporation, 1997.
CASR 23.. Airworthiness Standards: Normal, Utility, Acrobatic, and Commuter Category Airplanes. Indonesia: Ministry of Transportation.
M Sadraey, Aircraft Performance: Analysis; VDM Verlag Dr. Müller: Saarbrücken, Germany, 2011.
DOI: https://doi.org/10.47355/avia.v5i2.93
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