用于先进太空推进和深空任务的超导半低温燃料批判性评论

Panta Sasikanth
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引用次数: 0

摘要

探索深空需要革命性的推进技术,以克服所涉及的遥远距离。本综述对超导半低温燃料作为改变航天器推进方法的潜力进行了严格评估。超导体在低温下表现出零电阻,为高效电磁推力的产生提供了显著优势。然而,实现超导通常所需的超低温给航天器带来了后勤方面的挑战。本综述探讨了液氢和甲烷等半低温燃料的使用,从而在更易于管理的温度下运行,同时充分利用超导的优势。综述深入探讨了沸腾损失所带来的挑战,并分析了各种缓解技术,如多层绝缘、3M 玻璃气泡、主动冷却系统和零点沸腾(ZBO)。 此外,它还强调了超导半低温推进系统的潜在性能增益,包括显著减轻重量和提高效率。 此外,还讨论了辐射照射等关键考虑因素,以及进一步研究高温超导体和计算建模的必要性。 总之,本综述强调了超导半低温燃料为推进深空探索提供的大有可为的途径。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Critical Review on Superconducting Semi-Cryogenic Fuels for Advanced Space Propulsion and Deep Space Missions
The exploration of deep space necessitates revolutionary propulsion technologies to overcome the vast distances involved. This review critically evaluates the potential of superconducting semi-cryogenic fuels as a game-changing approach for spacecraft propulsion. Superconductors, exhibiting zero electrical resistance at low temperatures, offer significant advantages for efficient electromagnetic thrust generation. However, achieving the ultra-low temperatures typically required for superconductivity presents logistical challenges for spacecraft. This review explores the use of semi-cryogenic fuels like liquid hydrogen and methane, enabling operation at more manageable temperatures while leveraging the benefits of superconductivity. The review delves into the challenges of boil-off loss and analyzes various mitigation techniques like multilayer insulation, 3M glass bubbles, active cooling systems, and Zero Point Boil Off (ZBO).  Furthermore, it highlights the potential performance gains of superconducting semi-cryogenic propulsion systems, including significant weight reduction and improved efficiency.  Critical considerations such as radiation exposure and the need for further research in high-temperature superconductors and computational modeling are discussed.  Overall, this review underscores the promising path that superconducting semi-cryogenic fuels offer for advancing deep space exploration.
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