2021
DOI: 10.1109/access.2021.3057788
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Prospects and Challenges of the Hyperloop Transportation System: A Systematic Technology Review

Abstract: The present article outlines the core technologies needed to realize the Hyperloop transportation system (HTS). Currently, the HTS vacuum tube train concept is viewed as the fastest way to cross the earth's surface. However, the concept has not yet been demonstrated for subsonic or near-sonic speeds in large-scale implementations. Among the challenging technical areas are the tube's depressurization, the capsule's air resistance, and choked flows occurring around the capsule. There is also a need for effective… Show more

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Cited by 57 publications
(26 citation statements)
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“…A fruitful avenue for future research should be to examine how hyperloop transportation can be incorporated into Tesla's infrastructure network. Elon Musk describes it as a system which launches pods of passengers through tubes at high speed, yet its commercial feasibility remains to be technologically substantiated [51]. 1 .…”
Section: Discussionmentioning
confidence: 99%
“…A fruitful avenue for future research should be to examine how hyperloop transportation can be incorporated into Tesla's infrastructure network. Elon Musk describes it as a system which launches pods of passengers through tubes at high speed, yet its commercial feasibility remains to be technologically substantiated [51]. 1 .…”
Section: Discussionmentioning
confidence: 99%
“…The pod design significantly affects the design of the tube infrastructure, which depends on the loading pad configuration and the formation of distributed or concentrated loads [11], as well as the static, dynamic, and thermal loads [61]. The frontal surface and shape of the pod may affect the aerodynamic drag and the tube's operational energy consumption [5,14,28,31,36,39,51]. The Kantrowitz limit, the blockage ratio, the drag coefficient, and the pod's length are certain factors for optimizing the aerodynamic performance and pod speeds [5,18,22,24,26,27,34,41,43,51,60].…”
Section: The Pod 341 Structurementioning
confidence: 99%
“…The frontal surface and shape of the pod may affect the aerodynamic drag and the tube's operational energy consumption [5,14,28,31,36,39,51]. The Kantrowitz limit, the blockage ratio, the drag coefficient, and the pod's length are certain factors for optimizing the aerodynamic performance and pod speeds [5,18,22,24,26,27,34,41,43,51,60].…”
Section: The Pod 341 Structurementioning
confidence: 99%
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