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

Abstract

The patent application relates to a method of, and to an apparatus for, cutting, gr oves, and thereafter forming channels, in metal work pieces which have complex surfaces, and which are intended for use as components of a rocket engine.

Document Details

Document Type
Technical Report
Publication Date
Dec 21, 1973
Accession Number
AD0164701

Entities

People

  • D. G. Brown

Organizations

  • United States Department of the Air Force

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Composite Materials
  • Engines
  • Patent Applications
  • Patents
  • Rocket Engines
  • Rockets

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Electrical Engineering
  • Reinforced Composite Materials