Inventors:
Michel Roger Kamel - Montreal, Quebec H3M2S3, CA
Jacob Brian Lopata - Skokie IL 60076
International Classification:
F02K 964
US Classification:
60204, 60257, 60265, 2989001, 2391273
Abstract:
A rocket engine having a combustion chamber with a chamber inner wall, a throat with a throat inner wall, and a nozzle with a nozzle inner wall is provided. The chamber inner wall is a vacuum plasma sprayed metal, the throat inner wall is a vacuum plasma sprayed metal, and the nozzle inner wall is a vacuum plasma sprayed metal. The porosity of the vacuum plasma sprayed metal varies in an axial direction of the engine.