Sizing for battery powered, non-rigid, finless airship for low altitude application

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Sizing for battery powered, non-rigid, finless airship for low altitude application

A smaller airship with sub-100 kg payload capacity offers practical advantages, such as ease of operation, versatility, and reduced helium consumption. Payload weight significantly influences hull sizing and correlates with airship flight subsystems like power and propulsion. This paper presents a m...

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Bibliographic Details
Main Authors:	Mohd Harithuddin, Ahmad Salahuddin, Sedan, Mohd Fazri, Gires, Ezanee
Format:	Article
Published:	Aeronautical and Astronautical Society of the Republic of China, Taiwan 2024
Online Access:	http://psasir.upm.edu.my/id/eprint/110586/

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