Rocket nozzles in layered construction

Details Rocket nozzles in layered construction Rocket nozzles in layered construction

1985-11-21

1988-03-08

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

428408, B64D 3304

Patent

active

047295120

ABSTRACT:
An improved rocket nozzle liner for solid fuel rockets which is constructed from an inner liner of silicon carbide, a layer of highly anisotropic graphite and an outer shell of heat resistant material. The layer of anisotropic graphite permits thermal expansion of the silicon carbide, thus preventing the build up of thermal stresses and resulting fractures.

REFERENCES:
patent: 2658332 (1957-11-01), Nicholson
patent: 2706382 (1955-04-01), Logan et al.
patent: 3133411 (1964-05-01), McCorkle
patent: 3156091 (1964-10-01), Kraus
patent: 3224193 (1965-12-01), Loprote et al.
patent: 3313488 (1967-04-01), Lovingham
patent: 3639159 (1972-02-01), Rose et al.
patent: 3723214 (1973-03-01), Meraz
patent: 3900675 (1975-08-01), Olcott
patent: 3980105 (1976-09-01), Myskowski
patent: 4067956 (1978-01-01), Franklin et al.
patent: 4327868 (1982-05-01), Burkes, Jr.
patent: 4502983 (1985-03-01), Omori et al.
patent: 4621017 (1986-11-01), Chandler et al.

Affiliated with

Also associated with

Rating

Rocket nozzles in layered construction does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Rocket nozzles in layered construction, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Rocket nozzles in layered construction will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-227691