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Design of pipelines in high pressure LOX supply system
Author(s): 
Pages: 70-73
Year: Issue:  6
Journal: Journal of Rocket Propulsion

Keyword:  liquid rocket enginehigh pressure LOX supply systempipeline design;
Abstract: 高压液氧供应系统是我国压力最高的挤压式液体火箭发动机试验台的关键分系统。在系统设计过程中,通过合理布置管路,设计专用固定支架,采用自然补偿和堆积绝热技术,解决了高压低温推进剂系统管路设计中的难题。该系统顺利通过气密性检查和调试,经多次热试车考核,系统稳定可靠,满足设计要求。
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