Rocket nozzle snubber

Ordnance – Rocket launching – Underwater launching

Patent

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Details

60271, 23926511, F41F 307, B63H 1100

Patent

active

050605500

ABSTRACT:
Stress from the ignition of a rocket is transferred from the rocket nozzle o the actuators and flexible joint seal which move the nozzle causing potential failure of the actuators. This stress can be relieved by using a snubber in the form of a flexible hollow conical toroidal bladder filled with incompressible fluid fitted snugly between the nozzle and the main body of the rocket. Such a snubber transfers the stress to the main body of the rocket through the snubber while deforming to allow the rocket nozzle to slew in response to control commands.

REFERENCES:
patent: 3279192 (1966-10-01), Hull et al.
patent: 3568929 (1968-03-01), Butler et al.
patent: 4007586 (1977-02-01), McDermott
patent: 4949618 (1990-08-01), Tarlano
patent: 4967599 (1990-11-01), Donguy

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