THE THEORY OF ROCKET ENGINES.

Abstract

The subject of the book is the general theory and design of thermal rocket engines of various kinds. The writer discusses the operation, characteristics, and parameters of engines using chemical energy derived from liquid and solid rocket propellants. The book is intended for use as a textbook by students in colleges of aviation and other university-level institutions specializing in aircraft power plants. Engineers working in this field will also find it helpful. (Soviet editor's note)

Document Details

Document Type
Technical Report
Publication Date
Mar 20, 1964
Accession Number
AD0601547

Entities

People

  • V. E. Alemasov

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Books
  • Energetic Materials
  • Engineers
  • Engines
  • Materials
  • Propellants
  • Rocket Engines
  • Rocket Propellants
  • Rockets
  • Solid Rocket Propellants
  • Students
  • Thermal Propulsion Systems
  • Universities

Fields of Study

  • Physics

Readers

  • Internal Combustion Engine (ICE) Technology.
  • Library and Information Science
  • Theoretical Analysis.