Lockheed Martin Corporation

Eric Talley

William Davis Brokaw

Vladimir Volman

Wilhelmus H Theunissen

James Howard Sturges

Nathaniel David Cantor

William D Brokaw

A reflector support system is provided that includes a backing structure having a plurality of struts. The backing structure may have a plurality of hubs, each of the plurality of hubs may be configured to couple to two or more of the plurality of struts, each of the plurality of hubs may be configured to couple to another one of the plurality of hubs using one of the plurality of struts, each of the plurality of struts is configured to couple to at least two of the plurality of hubs. The backing structure may have a plurality of feet, each of the plurality of feet configured to couple to a corresponding one of the plurality of hubs, the plurality of feet are configured to couple to a reflector. In addition, a synthesis for mechanical adjustment of the reflector support system is provided.

Configurable backing structure for a reflector antenna and corrective synthesis for mechanical adjustment thereof

A high power radiating antenna system is disclosed which includes a ground plane and an electrically conductive power radiating element. The power radiating element includes a first, power feed end proximal to the ground plane and a second end distal to the ground plane. The power radiating element further includes an integrally formed heat pipe adapted for dissipating thermal energy generated in the power radiating element during operation of the antenna system.

Thermally dissipating high RF power radiating antenna system

A broadband mesh antenna and a phased array broadband mesh antenna are provided. The antenna of the present invention is a mesh antenna system that may be implemented with printed circuit board technology and wired technology that operates with increased bandwidth. The mesh antenna system provides for a single mesh antenna to operate at a wide range of frequencies. The antenna may be employed as a high efficient broadband antenna for rockets, space vehicles and ships when placed inside a metallic open box.

Broadband starfish antenna and array thereof

A deployable reflecting structure for use in space applications, preferably for RF antenna structures, includes at least one rigid section having a reflective surface and at least one bendable section having a reflective surface and being connected to the rigid section. The bendable section is movable between a first, stowed position in which the reflective surface of the bendable section is at least partially overlapping with the reflective surface of the rigid section, and a second, deployed position in which the reflective surfaces are continuous and non-overlapping.

Growing community of inventors

Hamilton, NJ, United States of America

Eric Talley