国外液体火箭发动机试验设施述评  

Review of test facilities for liquid rocket engines abroad

作　　者：罗维民[1] 

机构地区：[1]西安航天动力试验技术研究所,陕西西安710100

出　　处：《火箭推进》2015年第1期1-9,共9页Journal of Rocket Propulsion

摘　　要：对美国、俄罗斯、日本等国家及欧空局的液体火箭发动机试验设施、大推力发动机试验能力、高空模拟试验能力、试验设施测控能力、发动机边界条件与可靠性试验、吸气式动力装置试验、新型动力装置试验进行了较详细介绍。分析了国外液体火箭发动机试验设施、试验能力、试验技术和发展趋势,指出了我国液体动方试验设施、试验技术水平与国外存在的差距,对我国航天液体动力试验设施建设和技术发展方向,特别是重型运载火箭发动机和新型动力装置试验设施建设提供参考和借鉴。The test facilities, high-thrust engine test ability, space analog test ability, and engine boundary conditions, as well as reliability test, air-breathing power unit test and novel power unit test of liquid rocket engines in the United States of America, Russia, European Space Agency （ESA） and Japan are briefly introduced in this paper. The test facilities, test ability, test technologies and development tendency of foreign liquid rocket engines are analyzed. The gap between China and other advanced countries in the aspects of liquid power test facilities and test technology level is pointed out. The analysis of the test facilities for liquid rocket engines, especially for heavy lift rocket engines and novel power units in the world can be used as a reference for the test facility construction technological development in China.

关 键 词：液体火箭发动机试验设施 试验能力 试验技术 

分 类 号：V434-34[航空宇航科学与技术—航空宇航推进理论与工程]