Space Systems/loral, LLC

Victor Tam

George A Fiedziuszko

Robert N Seehorn

Hoover R Lee

Gary W White

A heat transfer interface is provided for radio-frequency resonator cavity filters used in vacuum environments such as are encountered by spacecraft and satellites. The heat transfer interface may include a thermally conductive structure that encircles or partially encircles a tubular structure of the resonator cavity filter and heat transfer legs that extend from positions that are on opposite sides of the thermally conductive structure and at approximately the same distance from a support surface to the support surface. The heat transfer legs and the thermally conductive structure may be made from a material or materials having a thermal conductivity of 350 W/(m&#xb7;K) or greater.

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San Bruno, CA, United States of America

Victor Tam