Exhaust dissipator device

Acoustics – Sound-modifying means – Muffler – fluid conducting type

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Details

181239, 181269, F02K 144

Patent

active

046855335

ABSTRACT:
An exhaust dissipator device for a rocket exhaust has an inlet for connection to the exhaust and a plurality of smaller exhaust orifices spaced around its surface to dissipate the flow into a plurality of smaller jets. A deflector surface in the direction of exhaust flow into the container acts to further dissipate the flow and deflect it out of its original path. This may comprise an internal surface of the container, or a separate deflector plate spaced from the container surface.

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