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Preliminary Sizing of High-Altitude Airships Featuring Atmospheric Ionic Thrusters: An Initial Feasibility Assessment

When it comes to computing the values of variables defining the preliminary sizing of an airship, a few standardized approaches are available in the existing literature. However, when including a disruptive technology in the design is required, sizing procedures need to be amended, so as to be able...

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Autori principali: Carlo E.D. Riboldi, Marco Belan, Stefano Cacciola, Raffaello Terenzi, Stefano Trovato, Davide Usuelli, Giuseppe Familiari
Natura: Artigo
Lingua:Inglês
Pubblicazione: MDPI AG 2024-07-01
Serie:Aerospace
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Accesso online:https://www.mdpi.com/2226-4310/11/7/590
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