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旋冷却热塑性室推进器,用于基于聚合物3D打印的空间推进系统的潜在应用
Mousa Aqailan1, Jeongmoo Huh2,3
1Department of Mechanical and Aerospace Engineering, College of Engineering, United Arab Emirates University, P.O. Box 15551, Al Ain, Abu Dhabi, United Arab Emirates.
Scientific reports
|August 14, 2025
概括
这项研究展示了一种新的旋冷却推进器,用于3D打印的航天器部件. 这项技术成功地保护了利用火星二氧化碳 (CO2) 作为资源的塑料燃烧室.
科学领域:
- * 航空航天工程 航空航天工程
- * 材料科学 材料科学
- * 化学工程 化学工程
背景情况:
- *火星上丰富的二氧化碳 (CO2) 为现场资源利用 (ISRU) 提供了机会.
- *将二氧化碳转化为塑料可以支持太空制造和3D打印推进系统.
- *热塑性材料为航天器部件的增材制造提供了潜力,但需要热管理解决方案.
研究的目的:
- * 为了研究一个旋冷却的热塑性燃烧室推进器的可行性.
- * 评估使用火星二氧化碳衍生塑料用于3D打印推进系统的可行性.
- * 为了评估热塑性推进器的热保护和推进性能,使用旋转冷却注射.
主要方法:
- *使用气和气态氧气的10N级双推进推进器被修改为热塑性燃烧室.
- * 实施了旋转式氧化剂注入,在室内表面沿着冷却层.
- * 进行了广泛的燃烧试验,以分析注射配置和质量流速对冷却性能的影响.
主要成果:
- *成功形成了稳定的冷却层,为塑料室提供了足够的热保护.
- *燃烧火焰保持在中心,温度超过室内材料的点火点.
- * 在各种注射配置中,特有的速度效率超过了大约80%.
结论:
- * 旋转冷却是一种可行的方法,用于热塑性燃烧室的热保护.
- *这项技术支持开发用于太空任务的基于聚合物的3D打印推进系统.
- *这些发现推动了使用ISRU进行可持续和适应性空间推进的增材制造.
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