Accession Number : AD0164641
Title : Composite Wall for a Regeneratively Cooled Thrust Chamber of a Liquid Propellant Rocket Engine.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C
Personal Author(s) : Huang,David H.
Report Date : 25 DEC 1973
Pagination or Media Count : 9
Abstract : The patent relates to a composite wall, and a method of manufacturing it, for a regeneratively cooled thrust chamber of a liquid propellant rocket engine. The composite wall of the thrust chamber comprises an outer wall component of high strength lightweight alloy, a middle wall component of nickel abutting with and joined to the outer wall component, and, an inner wall component of material of high thermal conductivity and high temperature strength and ductility, with the inner wall component abutting with and joined to the lands on the middle wall component.
Descriptors : *Liquid propellant rocket engines, *Thrust chambers, *Patents, Regenerative cooling, Fabrication, Structural members
Subject Categories : Liquid Propellant Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE