Accession Number : ADD004217

Title :   Method of Fabricating Combustion Chamber Liners.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON D C

Personal Author(s) : Couch,Harold Thompson ; cohen,Leonard Selwyn ; Coulter,Lawrence Joseph

Report Date : 28 Jun 1977

Pagination or Media Count : 6

Abstract : A fluid polymeric ablator liner is cast onto the inner surface of a ramjet combustion chamber which has been prepared with a screen liner substrate. A split mold is inserted through the nozzle and assembled inside the chamber allowing a thin layer of ablator to be cast and cured on the dome and nozzle regions of the combustion chamber. (Author)

Descriptors :   *Patents, *Combustion chamber liners, *Solid propellant rocket engines, Casting, Ablative materials, Nozzles

Subject Categories : Solid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE