航天器集成偏转护盾技术

Florian Neukart
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引用次数: 0

摘要

随着太空任务的速度和频率不断提高,有必要改进航天器保护技术,以确保任务的成功以及机载系统和人员的安全。现有的屏蔽解决方案包括电磁屏蔽、等离子体屏蔽和投射力场,每种方案都能提供独特的保护能力,但独立使用时都会受到限制。本研究提出了一种集成偏转护盾系统,该系统结合了这些技术的优势,可针对各种太空威胁(包括带电粒子、微流星体和高能辐射)提供全面保护。通过利用聚变能作为主要动力源,我们的目标是维持一个能够根据不同威胁程度进行动态调整的高能防护罩。广泛的理论建模、模拟和分析计算证明了这种综合方法的可行性,并突出了在能源效率和可扩展性方面的显著改进。这种多层防护罩系统的实施标志着航天器保护领域的一个关键进步,为更安全、更可靠的太空探索任务铺平了道路。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Integrated Deflector Shield Technology for Spacecraft
The increasing velocity and frequency of space missions necessitate advancements in spacecraft protection technologies to ensure mission success and the safety of onboard systems and personnel. Existing shielding solutions, including electromagnetic shields, plasma shields, and speculative force fields, each offer distinct protective capabilities but are limited when used independently. This study proposes an integrated deflector shield system that combines the strengths of these technologies to provide comprehensive protection against a wide range of spaceborne threats, including charged particles, micrometeoroids, and high-energy radiation. By leveraging fusion energy as a primary power source, we aim to sustain a high-energy shield capable of dynamically adjusting to varying threat levels. Extensive theoretical modeling, simulations, and analytical calculations demonstrate the feasibility of this integrated approach, highlighting significant improvements in energy efficiency and scalability. The implementation of this multi-layered shield system marks a pivotal advancement in spacecraft protection, paving the way for safer and more reliable space exploration missions.
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