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本文根据已经应用的系统和正在设计的系统的综合要求,介绍了用于火箭发动机上的离心泵。综述了流体动力与机械设计方面需要考虑的因素和技术问题以及试验方法。文章着重指出在泵的研制工作中存在的问题及其解决的办法。
In this paper, based on the system has been applied and the system is being designed synthesis requirements, introduced for the rocket engine centrifugal pump. The factors and technical problems to be considered in hydrodynamic and mechanical design and the test methods are reviewed. The paper emphatically points out the problems existing in the research and development of pumps and their solutions.