JPRS Report, Science & Technology, Japan, TRDI Technical Reports

Abstract

Partial contents: Characteristics of Double-Base Rocket Propellants; Performance of Argon-Xenon Laser; Burn Rate of Rocket Motors Reduced; Transonic Wind Tunnel Test To Evaluate Wing Flutter; Research on Lithium-Thionyl Chloride Batteries; Characteristics of New Lens Antenna; Two-Pulse Technique for New Rocket Motor.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
May 14, 1990
Accession Number
ADA335919

Entities

Organizations

  • Joint Publications Research Service

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Burning Rate
  • Chemical Reactions
  • Climate Change
  • Combustion
  • Composite Propellants
  • Double Base Propellants
  • Electric Discharges
  • Exothermic Reactions
  • Heat Transfer
  • Materials Laboratories
  • Materials Testing
  • Measurement
  • Nitrogen Oxides
  • Rocket Engines
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Battery Technology and Engineering
  • Rocket Propulsion.

Technology Areas

  • Directed Energy