航天推进技术研究院主办
[1]罗维民.国外液体火箭发动机试验设施述评[J].火箭推进,2015,41(01):1-9.
LUO Wei-min.Review of test facilities for liquid rocket engines abroad[J].Journal of Rocket Propulsion,2015,41(01):1-9.
点击复制
LUO Wei-min.Review of test facilities for liquid rocket engines abroad[J].Journal of Rocket Propulsion,2015,41(01):1-9.
国外液体火箭发动机试验设施述评
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
41
期数:
2015年01期
页码:
1-9
栏目:
专论与综述
出版日期:
2015-04-30
- Title:
- Review of test facilities for liquid rocket engines abroad
- 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
- 文献标志码:
- A
- 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，指出了我国液体动力试验设施、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。
- Abstract:
- 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.
参考文献/References:
[1]王永忠, РД-170发动机试验台[J]. 火箭推进, 2000 (3): 16-27.
[2]肖泽娟, 程惠尔, 周伟敏, 等，高空羽流试验系统和压力场的测量[J]. 上海交通大学学报, 2007 (9): 1542-1564.
[3]张斌章. 国外火箭发动机试车台及发展趋势研究[J]. 火箭推进, 2007 (5): 42-49.
[4]周军. LE-5和LE-7发动机的研制经验[J]. 火箭推进, 1997 (6): 45-55.
[5]张婵. 俄罗斯的液体火箭发动机研制企业-动力机械科研生产联合体[J]. 飞航导弹, 2000 (11): 34-35.
[6]来代初, 唐德芳, 赵万明. РД-120发动机试车台[J]. 火箭推进, 2004 (5): 20-26.
[7]祝敏. 分布式测控系统在发动机试验中的应用[J]. 火箭推进, 2013 (5): 98-102.
[8]BIANCO J. NASA Lewis Research Center's combustor test facilities and capabilities, AIAA 1995-2681[R]. USA: AIAA, 1995.
[9]MATRINGE L. PF52 test stand for the new VINCI rocket engine, AIAA 2001-3382[R]. USA: AIAA, 2001.
[10]KERL J M, SEVERT G A, LOOS K H. Advanced nozzle test facility at NASA Glenn Research Center, AIAA 2002-3245[R]. USA: AIAA, 2002.
[11]SHAMIM Rahman, BARTT Hebert. Rocket propulsion testing at Stennis Space Center current capability and future challenges, AIAA 2003-5038[R]. USA: AIAA, 2003.
[12]SHAMIM Rahman, BARTT Hebert. Large liquid rocket testing strategies and challenges, AIAA 2005-3564[R]. Tucson, USA: AIAA, 2005.
[13]GULLIA A, LASKARIDIS P. A preliminary investigation of thrust measurement correction in a enclosed engine test facility, AIAA 2005-1128[R]. Tucson, USA: AIAA, 2005.
[14]THOMAS E J,KERRY D K. Propulsion testing capabili- ties at NASA's John C. Stennis Space Center E-2 Cell 1 test facility, AIAA 2005-4419[R]. Tucson, USA: AIAA, 2005.
[15]HAMILTON J T. Marshall Space Flight Center test capa- bilities, AIAA 2005-4421[R]. Tucson, USA: AIAA, 2005.
[16]EMDEE J L. A survey of development test programs for LOX/kerosene rocket engines, AIAA 2001-3985[R]. USA: AIAA, 2001.
相似文献/References:
[1]李伟民.液氧/煤油发动机试验系统[J].火箭推进,2005,31(06):50.
Li Weimin.LOX/kerosene rocket engine test system[J].Journal of Rocket Propulsion,2005,31(01):50.
备注/Memo
收稿日期：2014-10-21；修回日期：2014-12-11 作者简介：罗维民（1962—），男，高级工程师，研究领域为液体火箭发动机试验技术
更新日期/Last Update:
1900-01-01