Journal of Chinese Society of Astronautics (Selected Articles)

Abstract

Contents: Research on Distribution of Size and Aggregate States of Burning Aluminum Droplets in Propellant Combustion; The Erosive Burning Characteristics of Aluminized Hipb Composite Propellant '87', The Action Mechanism of Lead Compounds in the Combustion Process of Double-Base Propellants. Chinese translations.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
May 02, 1989
Accession Number
ADA209144

Entities

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Burning Rate
  • Chemical Reaction Properties
  • Chemical Reactions
  • Combustion
  • Combustion Chambers
  • Combustion Products
  • Composite Propellants
  • Decomposition
  • Double Base Propellants
  • Erosive Burning
  • Ignition
  • Lead Oxides
  • Photographs
  • Photography
  • Propellants
  • Solid Propellants
  • Temperature Gradients

Fields of Study

  • Physics

Readers

  • Political Science/ International Relations/ European Studies
  • Rocket Propulsion.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster