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

Abstract

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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Document Details

Document Type
Technical Report
Publication Date
Feb 28, 1973
Accession Number
AD0760265

Entities

People

  • B. I. Borovskii
  • B. V. Ovsyannikov

Organizations

  • Air Force Systems Command

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Boundary Layer
  • Computational Fluid Dynamics
  • Energy Transfer
  • Fluid Dynamics
  • Fluid Flow
  • Gas Turbines
  • Geometric Forms
  • Guide Vanes
  • Heat Energy
  • Hydrodynamics
  • Materials Testing
  • Pressure Distribution
  • Radial Turbines
  • Rotor Blades (Turbomachinery)
  • Test And Evaluation
  • Thermodynamics

Fields of Study

  • Engineering
  • Physics

Readers

  • Aerodynamics.
  • Combustion science or combustion engineering.
  • Theoretical Analysis.