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国外电弧加热喷气火箭发动机理论与实验研究
Alternative TitleTHEORY AND EXPERIMENT ONARCJET ABROAD
吴汉基; 安世明; 刘宇; 张振鹏; 北京8701信箱
Department空间科学试验技术研究室
Source Publication推进技术
1994
Issue6Pages:61-67
ISSN1001-4055
Language中文
Keyword电弧喷射发动机 火箭发动机 推力控制
Abstract简要总结了国外电弧加热喷气火箭发动机研究发展的历史,介绍了实验研究系统的主要设备、发动机结构、零部件测量参数等,给出了实验研究的一些主要结果和结论,归纳了理论分析和数值分析的主要研究内容,并将电弧加热喷气火箭发动机气动热力学过程同化学火箭进行了比较。
Other AbstractThis paper makes a brief descreption about the research and developing history of arcjet abroad,introduces the main devices,the arcjet structure,the materials of its components and the measuring parameters,gives some principal resuits and conclusions of the test researches,sums up the primary contents of theory and numerical analysis about it,and makes a comparison between the thermodynamics and gas dynamics process of arejet and chemical rocket motor.
Funding Project中国科学院空间科学与应用研究中心
Document Type期刊论文
Identifierhttp://ir.nssc.ac.cn/handle/122/593
Collection空间技术部
Corresponding Author北京8701信箱
Recommended Citation
GB/T 7714
吴汉基,安世明,刘宇,等. 国外电弧加热喷气火箭发动机理论与实验研究[J]. 推进技术,1994(6):61-67.
APA 吴汉基,安世明,刘宇,张振鹏,&北京8701信箱.(1994).国外电弧加热喷气火箭发动机理论与实验研究.推进技术(6),61-67.
MLA 吴汉基,et al."国外电弧加热喷气火箭发动机理论与实验研究".推进技术 .6(1994):61-67.
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