COMMUNIST CHINESE ROCKET PROPULSION TECHNOLOGY: COMPILATION OF ABSTRACTS.

Abstract

This compilation of abstracts is based on CHICOM open sources published 1960-1966. It consists of 31 abstracts dealing with solid and liquid rocket propulsion technology. The abstracts are arranged alphabetically by author. Pertinent information included: shock-wave tube, thrust vector control and secondary injection for solid-propellant rockets, rocket materials (body and engine materials), chemical problems in combustion and flame, problems of rocket propellant chemistry, stress analysis of cast solid rocket grains, pyrometers, heat transfer in turbojet combustion chambers, film cooling effects, supersonic flow of nonequilibrium dissociating gas passing through a circular cone at an incidence angle, mathematical principles for rocket flights. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 11, 1966
Accession Number
AD0641892

Entities

Organizations

  • Library of Congress

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Chemistry
  • Combustion
  • Combustion Chambers
  • Film Cooling
  • Heat Transfer
  • Materials
  • Materials Science
  • Propellants
  • Rocket Propellant Grains
  • Rocket Propellants
  • Rocket Propulsion
  • Secondary Injection
  • Shock Waves
  • Solid Propellants
  • Stress Analysis
  • Supersonic Flow

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Dynamics.
  • Rocket Propulsion.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight