High Temperature Oxidation Resistance Coatings onAttitrde or Orbit Control Engine Thruster Chamber
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摘要:
概述了国内外姿/ 轨控液体火箭发动机高温抗氧化涂层的研究和应用进展,研制过程涉及多种材 料体系,但仅有几类广泛应用于型号,包括Nb 基材表面硅化物材料体系、Pt-Rh 合金、Re 基材表面Ir 涂层。随 着对发动机性能要求的提高,Re/ Ir 材料体系成为目前主要的研究方向。
Abstract:
The development and trend of high temperature oxidation resistance coatings on orbit or attitude con鄄 trol rocket engine are revieded . Silicide coatings on Nb alloy have been widely used from 1 960 s. Pt/ Rh alloy and Ir coating on Re are also applied on thruster chamber and Re/ Ir exhibit good performance above 2 000益, which is con鄄 sidered the best potential material.