建设可持续的火星基础设施:一个CO2呼吸等离子体推进器用于轨道维护和现场氧气生成
Anmol Taploo1, Guru Sankar Duppada1, Michael Keidar1
1Micro-Propulsion and Nanotechnology Laboratory, Department of Mechanical and Aerospace Engineering George Washington University Washington DC USA.
Global challenges (Hoboken, NJ)
|January 12, 2026
概括
这项研究介绍了用于火星任务的二氧化碳呼吸等离子体推进器,为火星任务提供电力推进和氧气生成. 它表现出超过1N的推力,支持未来在没有储存推进剂的情况下进行勘探.
科学领域:
- 太空飞船推进器 太空飞船推进器
- 行星科学 行星科学
- 等离子体物理学的物理学
背景情况:
- 未来的火星任务需要先进的推进和现场资源利用.
- 目前的推进系统通常依赖于储存的推进剂,限制任务持续时间和有效载荷.
研究的目的:
- 为了研究二重用途的二氧化碳 (CO2) 呼吸等离子体推进器,用于火星应用.
- 评估其在低火星轨道上进行电推进和现场氧气生成的能力.
主要方法:
- 一个二氧化碳呼吸等离子体推进器的实验测试.
- 在模拟的非常低的火星轨道 (80-160公里) 中运行.
- 使用光学发射光谱学分析推力性能和等离子体组成.
主要成果:
- 在0.1-1千瓦的输入功率下,达到超过1牛顿的推力.
- 通过强烈的777.1nm发射,证实了CO2在原子氧,一氧化碳 (CO) 和CO2中的有效解离.
- 在不同的放电频率中表现出功能.
结论:
- 二氧化碳呼吸等离子推进器是火星任务的可行的多功能平台.
- 能够实现电力推进和氧气生成,这对于空中/地面移动性和息地至关重要.
- 减少对储存推进剂的依赖,提高任务可行性和可持续性.
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