Abstract
小推力液体火箭发动机用铱/铼材料体系研究进展
Research Progress of Iridium/Rhenium Material System for Small Thruster
Received:September 02, 2013  
DOI:
中文关键词: 金属材料  铱/铼  火箭发动机  应用
英文关键词: metal materials  iridium/rhenium  thruster  application
基金项目:国家自然科学基金项目(50171031)资助。
Author NameAffiliationE-mail
CAI Hongzhong State Key Laboratory of Advanced Technologies for Comprehensive Utilization of Platinum Metals,Kunming Institute of Precious Metals, Kunming 650106, China chz@ipm.com.cn 
YI Jianhong Faculty of Materials and Engineering, Kunming University of Science and Technology, Kunming 650093, China  
WEI Yan State Key Laboratory of Advanced Technologies for Comprehensive Utilization of Platinum Metals,Kunming Institute of Precious Metals, Kunming 650106, China  
ZHENG Xu State Key Laboratory of Advanced Technologies for Comprehensive Utilization of Platinum Metals,Kunming Institute of Precious Metals, Kunming 650106, China  
QI Xiaohong State Key Laboratory of Advanced Technologies for Comprehensive Utilization of Platinum Metals,Kunming Institute of Precious Metals, Kunming 650106, China  
CHEN Li State Key Laboratory of Advanced Technologies for Comprehensive Utilization of Platinum Metals,Kunming Institute of Precious Metals, Kunming 650106, China  
HU Changyi State Key Laboratory of Advanced Technologies for Comprehensive Utilization of Platinum Metals,Kunming Institute of Precious Metals, Kunming 650106, China hcy@ipm.com.cn 
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中文摘要:
      概述了当前小推力液体火箭发动机用铱/铼材料体系研究和应用进展。随着对发动机性能要求的提高,研制出耐高温性能更好、质量更轻的新型铱/铼材料体系,并将它们应用于发动机燃烧室的制造是提高发动机技术水平的有效途径。
英文摘要:
      The development and trend ofiridium/rhenium material system for small thruster were summarized. With the request of improving the performance of small thruster, to develop and apply new lighter iridium/rhenium material system which has better high temperature performance is an effective way to improve the properties of the thrusters.
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