COOLED SOLID PROPELLANT ROCKET NOZZLES,

Abstract

A study was made to evaluate the potential of the liquid metal lithium as a coolant for solid propellant rocket nozzles. The program plan included the analysis, design, and testing of two cooling systems: Convection; and Spray film. A literature survey was made to review the state-of-the-art of rocket nozzle cooling (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 15, 1964
Accession Number
AD0602806

Entities

People

  • Sidney Elkind

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Convection
  • Gas Turbine Nozzles
  • Liquid Metals
  • Liquids
  • Literature
  • Literature Surveys
  • Nozzles
  • Propellants
  • Rocket Nozzles
  • Rockets
  • Solid Propellants

Fields of Study

  • Physics

Readers

  • Aerospace Propulsion Engineering.
  • Electrical Engineering
  • Internal Combustion Engine (ICE) Technology.