The patent application relates to the fabrication of propulsion components and to the resultant structures produced thereby. A multidimensional woven, resinous impregnated, rocket nozzle structure is 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.
Composite Rocket Nozzle Structure
1975
14 pages
Report
No indication
English
Composite Rocket Nozzle Structure
NTIS | 1975
|Rocket nozzle assembly and assembling method of rocket nozzle assembly
European Patent Office | 2025
NTIS | 1977
|Engineering Index Backfile | 1962
|