Accession Number : AD0164701

Title :   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.

Descriptive Note : Patent Application,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Personal Author(s) : Brown,D. G.

Report Date : 21 DEC 1973

Pagination or Media Count : 16

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.

Descriptors :   *Liquid propellant rocket engines, *Combustion chambers, *Electroerosive machining, Patents, Regenerative cooling, Spark machining, Cutting tools, Machines

Subject Categories : Mfg & Industrial Eng & Control of Product Sys
      Machinery and Tools
      Liquid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE