Rocket motor extendible nozzle exit cone

Details Rocket motor extendible nozzle exit cone Rocket motor extendible nozzle exit cone

1986-10-10

1988-11-29

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

With means controlling amount, shape or direction of...

F02K 108

Patent

active

047875593

ABSTRACT:
A rocket motor extendible nozzle is made by folding a sheet stock (metal, etc.) development of a membrane in the form of a cone or conical frustum (with a straight meridian) in such manner that the aft or larger diameter region of the membrane that is constructed by joining the two longitudinal edges may be collapsed for stowage with vastly reduced overall length, maximum diameter, and with substantially increased rigidity in comparison with the fully deployed unit. In the stowed condition, the material comprising the aft portion of the membrane is situated in multiple layers within the forward portion so that deployment is induced by forward-to-aft gas flow of the rocket motor within the cone.

REFERENCES:
patent: 3596465 (1971-08-01), Paine
patent: 3615052 (1971-10-01), Tumavicus
patent: 4272956 (1981-06-01), Lamere et al.
patent: 4349155 (1982-09-01), Donguy
patent: 4387564 (1983-06-01), Carey
patent: 4426038 (1984-01-01), Inman et al.
patent: 4638947 (1987-01-01), Jaqua et al.

Affiliated with

Also associated with

Rating

Rocket motor extendible nozzle exit cone 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 motor extendible nozzle exit cone, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Rocket motor extendible nozzle exit cone will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-358391