Abstract
High-temperature superconductor (HTS) materials, including HTS wires and bulks, become available to apply in transportation applications such as various hybrid levitation and linear propulsion systems. In this paper, for the evacuated tube transportation and electromagnetic aircraft launch system applications, two different types of hybrid HTS levitation and linear propulsion systems have been designed and modeled, respectively. The levitation force and electromagnetic thrust performance of the systems have been studied by a numerical and finite element method. With the principal parameters' verification, this work forms a basis for the structural and electromagnetic design of a hybrid HTS levitation and linear propulsion systems for practical hyper flight applications.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
