Levitation characteristics of a high-temperature superconducting Maglev system for launching space vehicles
โ Scribed by Wenjiang Yang; Yu Liu; Xiaodong Chen; Zheng Wen; Yi Duan; Ming Qiu
- Publisher
- Elsevier Science
- Year
- 2007
- Tongue
- English
- Weight
- 699 KB
- Volume
- 455
- Category
- Article
- ISSN
- 0921-4534
No coin nor oath required. For personal study only.
โฆ Synopsis
Maglev launch assist is viewed as an effective method to reduce the cost of space launch. The primary aerodynamic characteristics of the Maglev launch vehicle and the space vehicle are discussed by analyzing their aerodynamic shapes and testing a scale mode in a standard wind tunnel. After analyzing several popular Maglev systems, we present a no-controlling Maglev system with bulk YBaCuO high-temperature superconductors (HTSs). We tested a HTS Maglev system unit, and obtained the levitation force density of 3.3 N/cm 2 and the lateral force density of 2.0 N/cm 2 . We also fabricated a freely levitated test platform to investigate the levitation characteristics of the HTS Maglev system in load changing processes. We found that the HTS system could provide the strong self-stable levitation performance due to the magnetic flux trapped in superconductors. The HTS Maglev system provided feasibility for application in the launch vehicle.
๐ SIMILAR VOLUMES
A high rigidity type superconducting magnet (SCM) is developed and tested by an electromagnetic vibration simulator which simulates the actual running conditions. To reduce the increase in heat load due to the vibration of the cryostat, several kinds of design concepts are chosen. It is recognized f
Recently, for improvement of the magnetic field of high temperature superconductor (HTS) apparatus, many studies on operating in the temperature range of 20-65 K with liquid helium or the thermal conducting method using cryocooler are actively reviewed. Also, the cooling method of using solid nitrog