Assessment of the range of an electric aircraft

Electrification of aircraft is a rapidly developing area of the aerospace industry. Thus, there are many electric aircrafts in development, testing, or production. Electric aircrafts are currently viable for short range and short time flight missions due to battery-specific energy limitations. Hence...

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Main Author: Idres, Moumen Mohammed Mahmoud
Format: Article
Language:English
English
Published: Semarak Ilmu Publishing 2024
Subjects:
Online Access:http://irep.iium.edu.my/115685/7/115685_Assessment%20of%20the%20Range%20of%20an%20Electric%20Aircraft.pdf
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spelling my.iium.irep.1156852024-11-11T07:56:02Z http://irep.iium.edu.my/115685/ Assessment of the range of an electric aircraft Idres, Moumen Mohammed Mahmoud T Technology (General) TL Motor vehicles. Aeronautics. Astronautics TL500 Aeronautics Electrification of aircraft is a rapidly developing area of the aerospace industry. Thus, there are many electric aircrafts in development, testing, or production. Electric aircrafts are currently viable for short range and short time flight missions due to battery-specific energy limitations. Hence, training and commuter aircrafts are feasible targets for electrification. Pipistrel Velis Electro is the world's first certified crewed electric aircraft for pilot training. In this work, Pipistrel Velis Electro aircraft range is evaluated based on solution of longitudinal equations of motion. A simple flight mission that includes take-off, climb, cruise, descent and landing is considered. Electric propulsion components are modelled. The predicted range of the aircraft is 63 nm for a flight time of 43 minutes, which matches favourably with aircraft published data. The study showed that the Breguet range equation overestimates range, particularly at high altitudes. Hence, the proposed approach in this article is necessary for accurate prediction of range for short-range aircraft. Battery capacity-payload-range charts are developed for present and future battery technologies. Aircraft range can be extended to 150 nm if battery capacity is increased to 166 Ah and the payload is only the pilot. Doubling battery specific energy would extend the range to 193 nm with a flight time of 130 minutes. Semarak Ilmu Publishing 2024-08-25 Article PeerReviewed application/pdf en http://irep.iium.edu.my/115685/7/115685_Assessment%20of%20the%20Range%20of%20an%20Electric%20Aircraft.pdf application/pdf en http://irep.iium.edu.my/115685/13/115685_Assessment%20of%20the%20Range%20of%20an%20Electric%20Aircraft_Scopus.pdf Idres, Moumen Mohammed Mahmoud (2024) Assessment of the range of an electric aircraft. Journal of Advanced Research in Applied Sciences and Engineering Technology, 50 (2). pp. 155-170. E-ISSN 2462-1943 http://semarakilmu.com.my/journals/index.php/applied_sciences_eng_tech/article/view/5234 10.37934/araset.50.2.155170
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
language English
English
topic T Technology (General)
TL Motor vehicles. Aeronautics. Astronautics
TL500 Aeronautics
spellingShingle T Technology (General)
TL Motor vehicles. Aeronautics. Astronautics
TL500 Aeronautics
Idres, Moumen Mohammed Mahmoud
Assessment of the range of an electric aircraft
description Electrification of aircraft is a rapidly developing area of the aerospace industry. Thus, there are many electric aircrafts in development, testing, or production. Electric aircrafts are currently viable for short range and short time flight missions due to battery-specific energy limitations. Hence, training and commuter aircrafts are feasible targets for electrification. Pipistrel Velis Electro is the world's first certified crewed electric aircraft for pilot training. In this work, Pipistrel Velis Electro aircraft range is evaluated based on solution of longitudinal equations of motion. A simple flight mission that includes take-off, climb, cruise, descent and landing is considered. Electric propulsion components are modelled. The predicted range of the aircraft is 63 nm for a flight time of 43 minutes, which matches favourably with aircraft published data. The study showed that the Breguet range equation overestimates range, particularly at high altitudes. Hence, the proposed approach in this article is necessary for accurate prediction of range for short-range aircraft. Battery capacity-payload-range charts are developed for present and future battery technologies. Aircraft range can be extended to 150 nm if battery capacity is increased to 166 Ah and the payload is only the pilot. Doubling battery specific energy would extend the range to 193 nm with a flight time of 130 minutes.
format Article
author Idres, Moumen Mohammed Mahmoud
author_facet Idres, Moumen Mohammed Mahmoud
author_sort Idres, Moumen Mohammed Mahmoud
title Assessment of the range of an electric aircraft
title_short Assessment of the range of an electric aircraft
title_full Assessment of the range of an electric aircraft
title_fullStr Assessment of the range of an electric aircraft
title_full_unstemmed Assessment of the range of an electric aircraft
title_sort assessment of the range of an electric aircraft
publisher Semarak Ilmu Publishing
publishDate 2024
url http://irep.iium.edu.my/115685/7/115685_Assessment%20of%20the%20Range%20of%20an%20Electric%20Aircraft.pdf
http://irep.iium.edu.my/115685/13/115685_Assessment%20of%20the%20Range%20of%20an%20Electric%20Aircraft_Scopus.pdf
http://irep.iium.edu.my/115685/
http://semarakilmu.com.my/journals/index.php/applied_sciences_eng_tech/article/view/5234
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score 13.214268