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Optimization and Analysis of an Elite Electric Propulsion System

Mehakveer Singh et al · Embry-Riddle Aeronautical University · 2019

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<p><strong><em>Abstract- Electric propulsion has a promising system to create new possibilities in this technological era as well as control the harmful gaseous emission. This paper put a vision on several parameters of electric propulsion. The engine’s performance is comparable to the current propulsion devices and provides a lightweight solution to the robust technologies’ dependent on chemical energy sources. There are a plethora of factors which is enhanced by electric propulsion such as, overall efficiency, capabilities, and robustness of future air vehicles as well as mainly overcome from exhaust hazards. Electric propulsion systems have the potential of utilizing the electrically-driven propulsion system which is coupled electrically to power-generating devices. As a result, the electric propulsion system operated with greater flexibility and the synergistic benefits of aero-propulsive coupling and enhance performance in comparison with traditional designs. The experimentally calculated thrust of the engine model is approximately 547.6365, Newton.</em></strong></p>

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APA 7

al, M. S. E. (2019). Optimization and Analysis of an Elite Electric Propulsion System. https://doi.org/10.15394/ijaaa.2019.1419

MLA

al, Mehakveer Singh et. "Optimization and Analysis of an Elite Electric Propulsion System." 2019. https://doi.org/10.15394/ijaaa.2019.1419.

Chicago

al, Mehakveer Singh et. 2019. "Optimization and Analysis of an Elite Electric Propulsion System.". https://doi.org/10.15394/ijaaa.2019.1419.

Harvard

al, M. S. E. 2019, Optimization and Analysis of an Elite Electric Propulsion System, Embry-Riddle Aeronautical University, available at: https://doi.org/10.15394/ijaaa.2019.1419 [Accessed 7 Aug. 2026].

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Title
Optimization and Analysis of an Elite Electric Propulsion System
Author / contributors
Mehakveer Singh et al
Publisher
Embry-Riddle Aeronautical University
Publication year
2019
ISSN
2374-6793
ISSN
2374-6793
Language
English

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