Rocket Engines on a Combined Fuel

Abstract

Contents: General information about combined rocket engines; Heat exchange in the combustion chamber of combined rocket engines; Heterogeneous burning in the combined rocket engine; Selection of the basic parameters of combustion chamber of a combined rocket engine; Static characteristics of combined rocket engines; The control of combined rocket engines.

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Document Details

Document Type
Technical Report
Publication Date
Jun 24, 1974
Accession Number
AD0783752

Entities

People

  • E. B. Volkov
  • G. Yu. Mazing

Organizations

  • Air Force Systems Command

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Birds
  • Boundary Layer
  • Combustion
  • Combustion Products
  • Control Systems
  • Crystal Structure
  • Fluid Flow
  • Heat Energy
  • Heat Transfer
  • Ignition
  • Latent Heat
  • Liquid Propellant Rocket Engines
  • Materials Laboratories
  • Rocket Engines
  • Rocket Oxidizers
  • Specific Heat
  • Test And Evaluation

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Combustion science or combustion engineering.