航天推进技术研究院主办
液氧/甲烷液体火箭发动机燃烧研究最新进展
- Title:
- Recent Advances on LOX/Methane Combustion for Liquid Rocket Engine
- 分类号:
- V434
- 文献标志码:
- A
- 摘要:
- 近来,俄罗斯和欧洲正在联合进行一个名为“VOLGA”的研究计划。其主要目标是用于可重复使用运载火箭或大型助推器的液氧/甲烷发动机的概念研究。SNECMA 的主要工作是研究预燃室/燃气发生器的可重复使用技术,在液氧/液氢“火神”燃气发生器研制过程中,获得了很多低温推进剂的燃烧经验,但液氧/甲烷富燃燃烧带来了许多新的问题:如喷注性能、燃烧效率、稳定性、积碳形成等。为了解决上述问题,目前正在进行实验和理论两方面的研究。ONERA 的马斯喀特(Mascotte)试验装置就被改造用于研究甲烷的燃烧。最初的研究完成了
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