Theory and Calculation of Feed Units of Liquid-Propellant Rocket Engines,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
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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.
- Pumps, Filters, Pipes, Tubing, Fittings and Valves
- Liquid Propellant Rocket Engines