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

• 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/; https://www.airitilibrary.com/Article/Detail/P20140627004-N202403020027-00033

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...