可持续的太空技术 - - 针对可重复使用的太空运输系统的预测性气热设计的战略
Sebastian Karl1, Tamas Bykerk1
1German Aerospace Center, DLR, Institute of Aerodynamics and Flow Technology, Bunsenstraße 10, 37073 Göttingen, Germany.
The Review of scientific instruments
|February 11, 2024
概括
这篇评论涵盖了航天器的气热设计,分析了火箭,滑翔机和囊中的挑战. 它强调了当前的局限性,并提出了高效,可重复使用的空间运输系统的战略.
科学领域:
- 航空航天工程 航空航天工程
- 热力学是一种热力学.
- 计算流体动力学的流体动力学.
背景情况:
- 航天器的设计涉及到大气进入和上升过程中复杂的气热挑战.
- 了解高温热力学,化学动力学和辐射对于任务的成功至关重要.
研究的目的:
- 对各种航天器架构的当前气热设计和分析方法进行审查.
- 识别现有的数值和实验工具中的局限性和不确定性.
- 为可重复使用空间运输系统的高效气热设计提出未来战略.
主要方法:
- 对现有的关于航天器气热设计和分析的文献进行审查.
- 讨论不同忠实度级别的数值和实验工具.
- 分析物理现象,包括高温热力学,化学效应,流,辐射和气体动力学.
主要成果:
- 关键航天器系统架构 (火箭,滑翔机,囊) 的概述.
- 在飞行过程中识别特定的气热和热化学效应.
- 在预测模型中评估当前的局限性和不确定性来源.
结论:
- 当前的气热模型在预测复杂的物理现象方面存在局限性.
- 需要进一步的研究来增强航天器设计的预测能力.
- 为开发高效,可重复使用的太空运输系统提出了战略方法.
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