Accession Number : ADD004550

Title :   Composite Rocket Nozzle Structure.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Personal Author(s) : O'Brien,John R ; Holman,Harry A , Jr ; Kallmeyer,W

Report Date : 20 Dec 1977

Pagination or Media Count : 5

Abstract : A multidimensional woven, resinous impregnated, rocket nozzle structure composed of fibers running along the longitudinal axis of the nozzle and positioned radially in conformance with the general shape of the nozzle with a weaving Fiber under tension and running circumferentially and radially normal to the said longitudinal axis to interlock with said longitudinal fibers in at least three directions. (Author)

Descriptors :   *Rocket nozzles, *Composite materials, *Patents, Weaving

Subject Categories : Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE