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。
The development and trend of iridium/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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