Composite rocket nozzle structure

Details Composite rocket nozzle structure Composite rocket nozzle structure

1975-11-25

1977-12-20

Dixon, Jr., William R.

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

239DIG19, 428 36, 428102, 428113, 428251, 428257, 428273, 428902, B63H 1100, B64D 3304

Patent

active

040636844

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.

REFERENCES:
patent: 2948950 (1960-08-01), Finger et al.
patent: 3466210 (1969-09-01), Wareham
patent: 3713934 (1973-01-01), Morton
patent: 3719212 (1973-03-01), Emerson et al.
patent: 3750714 (1973-08-01), Holman et al.
patent: 3819461 (1974-06-01), Saffadi
patent: 3853586 (1974-12-01), Olcott
patent: 3875973 (1975-04-01), Kallmeyer et al.
patent: 3902944 (1975-09-01), Ashton et al.
patent: 4001478 (1977-01-01), King
Barton, "A Three Dimensionally Reinforced Material," Society of Plastics Engineers Journal, vol. 24, May 1968, pp. 31-36.
Robbins, "Structural Components Produced by Modified Weaving Techniques", Textile Institute and Industry, Mar. 1970, pp. 71-75.
Emerson, "Modern Developments in Three-Dimensional Fabrics", Modern Textiles, Nov. 1969, pp. 51-54.

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