Attenuation ring

Aeronautics and astronautics – Spacecraft – With fuel system details

Patent

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Details

244 63, 248573, 248634, 2671413, B64G 164

Patent

active

058789804

ABSTRACT:
An attenuation ring assembly for mounting between the payload section and the booster section of a launch vehicle is disclosed. The ring assembly acts as a transient filter to delete or minimize harmful shock and vibration frequencies which might otherwise reach and possibly damage delicate electronic components and the like in the launch vehicle payload.

REFERENCES:
patent: 3167294 (1965-01-01), Andrews et al.
patent: 4682744 (1987-07-01), Gounder
patent: 4755154 (1988-07-01), Ewbank
patent: 5389746 (1995-02-01), Moody
patent: 5529264 (1996-06-01), Bedegrew et al.

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