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Theory and Calculation of Feed Units of Liquid-Propellant Rocket Engines.

机译：液体火箭发动机进给装置的理论与计算。

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摘要

In the book information on the theory and hydraulic design of pumps and turbines of turbopump units (TU) (THA) of liquid-propellant rocket engines (LPRE) is given. Principles of the general theory of vane machines are given. The basic calculated relations for the design of the flow part of pumps and turines are derived. The selection of the basic parameters of turbopump units is substantiated, and conditions of their operation are analyzed. Methods of the calculation of pumps and turbines of LPRE are briefly set forth. Examples of the calculation are given.

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作者
Ovsyannikov, B. V.; Borovskii, B. I.;
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年度 1973
页码 1-793
总页数 793
原文格式 PDF
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关键词
Turbopumps; Rocket motors(Liquid propellant); Propellant control; Performance(Engineering); Configuration; Cascade structures; Turbine parts; Centrifugal pumps; Propeller pumps; Cavitation; USSR; Translations;

机译：涡轮泵;火箭发动机（液体推进剂）;推进剂控制;性能（工程）;配置;级联结构;涡轮机部件;离心泵;螺旋桨泵;空化;苏联;翻译;

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机译：液体火箭发动机。液体火箭发动机和动力装置理论原理

Theory and Calculation of Feed Units of Liquid-Propellant Rocket Engines.

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