Pressurised Fuel Vessel Mass Estimation for High-Altitude PEM Unmanned Aircraft Systems
The power to weight ratio of power plants is an important consideration, especially in the design of Unmanned Aircraft System (UAS). In this paper, a UAS with an MTOW of 35.3 kg, equipped with a fuel cell as a prime power supply to provide electrical power to the propulsion system, is considered. A...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2025-04-01
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| Series: | Fuels |
| Subjects: | |
| Online Access: | https://www.mdpi.com/2673-3994/6/2/26 |
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