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Hydrogen-powered Aircraft: Fundamental Concepts, Key Technologies, and Environmental Impacts

Abstract

Civil aviation provides an essential transportation network that connects the world and supports global economic growth. To maintain these benefits while meeting environmental goals, next-generation aircraft must have drastically reduced climate impacts. Hydrogen-powered aircraft have the potential to fly existing routes with no carbon emissions and reduce or eliminate other emissions. This paper is a comprehensive guide to hydrogen-powered aircraft that explains the fundamental physics and reviews current technologies. We discuss the impact of these technologies on aircraft design, cost, certification, and environment. In the long term, hydrogen aircraft appear to be the most compelling alternative to today’s kerosene-powered aircraft. Using hydrogen also enables novel technologies, such as fuel cells and superconducting electronics, which could lead to aircraft concepts that are not feasible with kerosene. Hydrogen-powered aircraft are technologically feasible but require significant research and development. Lightweight liquid hydrogen tanks and their integration with the airframe is one of the critical technologies. Fuel cells can eliminate in-flight emissions but must become lighter, more powerful, and more durable to make large, fuel cell-powered transport aircraft feasible. Hydrogen turbofans already have these desirable characteristics but produce some emissions, albeit much less damaging than kerosene turbofans. Beyond airframe and propulsion technologies, the viability of hydrogen aircraft hinges on low-cost green hydrogen production, which requires massive investments in the energy infrastructure.

Funding source: The first author is supported by the Department of Defense through the National Defense Science and Engineering Graduate (NDSEG) Fellowship Program, United States. He is also supported in part by the Michigan Institute for Computational Discovery and Engineering (MICDE) Graduate Fellowship program, United States. The second author was partially supported by NASA, United States through grant number F060365 of the Advanced Air Transport Technology (AATT) and Transformational Tools and Technologies (TTT) projects.
Related subjects: Applications & Pathways
Countries: United States
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/content/journal6326
2024-09-19
2024-12-18
/content/journal6326
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