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. (Author)
Composite Rocket Nozzle Structure
1975
5 pages
Report
Keine Angabe
Englisch
Composite Rocket Nozzle Structure
NTIS | 1975
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