THEORETICAL BASES FOR THE DESIGN OF LIQUID-FUELED ROCKET ENGINES

Abstract

Theoretical foundations of the design of liquid fueled rocket engines are given using data published in the foreign literature as a basis. The operating modes, working processes, and characteristics of the liquid-fueled rocket engine and its chamber, the planning and design of atomizing devices and systems for delivering fuel into the chamber, as well as the specifications of the fuels used are discussed. The book also illuminates the problems of chamber cooling and operation and testing of liquid-fueled rocket engine. The volume is designed as a study aid for the higher technical schools in the corresponding specialties: it can also be used as a textbook for engineers and technicians in this field.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Mar 07, 1962
Accession Number
AD0273887

Entities

People

  • M.i. Shevelyuk

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Calorific Value
  • Chemical Synthesis
  • Chemistry
  • Heat Energy
  • Heat Transfer
  • Material Degradation Processes
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Materials Testing
  • Thermodynamics

Readers

  • Business Analytics
  • Combustion and Flow Dynamics.
  • Instructional Design and Training Evaluation.