Non-radiating extendible cloth exit cone for rocket nozzles

Details Non-radiating extendible cloth exit cone for rocket nozzles Non-radiating extendible cloth exit cone for rocket nozzles

1982-01-11

1984-01-17

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

With erodible, frangible or fusible nozzle part

60271, 602001, 23926543, 239DIG19, B64D 3304

Patent

active

044260385

ABSTRACT:
A non-radiating cloth exit cone for a rocket nozzle includes a flared woven refractory cloth structure having the shape of the frustum of a cone with a refractory felt sewn to the exterior surface of the cloth structure for thermal insulation of the cloth structure and a sacrificial ablative material comprising tufts of refractory material incorporated in the interior surface of the cloth structure, the cloth structure providing the primary supporting structure for transmitting the rocket motor thrust forces to the rocket nozzle.

REFERENCES:
patent: 3358933 (1967-12-01), Altseimer
patent: 3482783 (1969-12-01), Nebiker et al.
patent: 3596465 (1971-08-01), Paine
patent: 3648461 (1972-03-01), Bailey et al.
patent: 3711027 (1973-01-01), Carey
patent: 3784109 (1974-01-01), Dueringer
patent: 3933310 (1976-01-01), Hickox
patent: 3957206 (1976-05-01), Mason
patent: 4162040 (1979-07-01), Carey

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