Solid-Propellant Rocket Engines,

Abstract

The book describes the motion of combustion products in the chamber and nozzle of solid-propellant rocket engine. The spreads of intrachamber and output characteristics of RDTT, caused by random and systematic deviations of the loading parameters are analyzed. The effect of the engine and propellant characteristics on the ideal velocity of the rocket is also analyzed. The book also examines the procedure for profiling of nozzles, the motion of two-phase combustion products, and the calculation and design of charges from solid rocket propellants.

Document Details

Document Type
Technical Report
Publication Date
Apr 09, 1974
Accession Number
AD0780834

Entities

People

  • A. M. Vinitskii

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Combustion
  • Combustion Products
  • Engines
  • Propellants
  • Rocket Engines
  • Rocket Propellants
  • Rockets
  • Solid Propellant Rocket Engines
  • Solid Propellants
  • Solid Rocket Propellants

Fields of Study

  • Physics

Readers

  • Business Analytics
  • Rocket Propulsion.