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