Method of, and Apparatus for Forming Grooves and Coolant Channels in and for Rocket Engine Composite Channel-Type Coolant Wall Having a Complex Surface.

Abstract

The patent application relates to a spark discharge device designed to simultaneously cut multiple coolant grooves in rocket engine combustion chambers.

Document Details

Document Type
Technical Report
Publication Date
Aug 08, 1972
Accession Number
AD0164471

Entities

People

  • Donald E. Brown

Organizations

  • United States Department of the Air Force

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Chambers
  • Chemical Reactions
  • Combustion
  • Combustion Chambers
  • Composite Materials
  • Engines
  • Exothermic Reactions
  • Heat Engines
  • Heat Transfer Devices
  • Ignition
  • Internal Combustion Engines
  • Patent Applications
  • Patents
  • Rocket Engines
  • Rockets

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Reinforced Composite Materials