THERMODYNAMIC AND BALLISTIC DESIGN FUNDAMENTALS OF SOLID-PROPELLANT ROCKET ENGINES,

Abstract

In this book, on the basis of materials published in the Soviet and foreign press, there are expounded thermo-gas-dynamic principles of designing of rocket engines, engineering methods of calculation of processes of heat exchange, principles of the theory of burning of solid fuels and calculation of the indicated pressure curve in the combustion chamber of the engine. In it there is given basic information about solid rocket propellants applied in solid-propellant rocket engines (SPRE). There is considered regulation of thrust in SPRE in magnitude and direction, and also a general method of ballistic designing of solid-fuel rockets. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 16, 1966
Accession Number
AD0645793

Entities

People

  • B. V. Orlov
  • G. Yu. Mazing

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Chambers
  • Combustion
  • Combustion Chambers
  • Engines
  • Fuels
  • Materials
  • Propellants
  • Rocket Engines
  • Rocket Propellants
  • Rockets
  • Solid Fuels
  • Solid Propellant Rocket Engines
  • Solid Propellants
  • Solid Rocket Propellants

Fields of Study

  • Physics

Readers

  • Library and Information Science
  • Rocket Propulsion.
  • Systems Analysis and Design