Peters Adam B, Zhang Dajie, Chen Samuel, Ott Catherine, Oses Corey, Curtarolo Stefano, McCue Ian, Pollock Tresa M, Eswarappa Prameela Suhas
Department of Materials Science and Engineering, Johns Hopkins University, Baltimore, MD, 21218, USA.
Johns Hopkins Applied Physics Laboratory, Laurel, MD, 20723, USA.
Nat Commun. 2024 Apr 18;15(1):3328. doi: 10.1038/s41467-024-46753-3.
Hypersonic vehicles must withstand extreme conditions during flights that exceed five times the speed of sound. These systems have the potential to facilitate rapid access to space, bolster defense capabilities, and create a new paradigm for transcontinental earth-to-earth travel. However, extreme aerothermal environments create significant challenges for vehicle materials and structures. This work addresses the critical need to develop resilient refractory alloys, composites, and ceramics. We will highlight key design principles for critical vehicle areas such as primary structures, thermal protection, and propulsion systems; the role of theory and computation; and strategies for advancing laboratory-scale materials to manufacturable flight-ready components.
高超音速飞行器在超过音速五倍的飞行过程中必须承受极端条件。这些系统有可能促进快速进入太空、增强防御能力,并为跨大陆地对地旅行创造新的模式。然而,极端的气动热环境给飞行器的材料和结构带来了重大挑战。这项工作满足了开发具有弹性的难熔合金、复合材料和陶瓷的迫切需求。我们将重点介绍关键飞行器部件(如主要结构、热防护和推进系统)的关键设计原则;理论和计算的作用;以及将实验室规模的材料推进到可制造的适航部件的策略。