Abstract: An electrically conductive filler comprises particles having a base substrate and a conductive coating. In some embodiments, the base substrate is a metal, plastic, glass, natural or synthetic graphite, carbon, ceramics, fiber or fabric. In some embodiments, the coating provides improved electrical conductivity, and the coated particle has lower electrical resistance than the uncoated base particle. Other embodiments and methods of making and using the electrically conductive filler are also disclosed.

Abstract: Conductive, lightweight, corrosion-resistant fiber mats are described herein. More particularly a metalized fiber mat of non-woven fibers has a conductive metal coating of a uniform thickness and a corrosion-resistant metal coating of a uniform thickness. Methods of producing such fiber mats are also provided.

Abstract: An electrically conductive filler comprises particles having a base substrate and a conductive coating. In some embodiments, the base substrate is a metal, plastic, glass, natural or synthetic graphite, carbon, ceramics, fiber or fabric. In some embodiments, the coating provides improved electrical conductivity, and the coated particle has lower electrical resistance than the uncoated base particle. Other embodiments and methods of making and using the electrically conductive filler are also disclosed.

Abstract: The invention relates to the use of amino terminated phosphonamides and their oligomers, as flame retardant additives for a variety of polymers to impart flame retardancy while maintaining or improving processing characteristics and other important properties.

Abstract: The invention relates to the use of amino terminated phosphonamides and their oligomers, as flame retardant additives for a variety of polymers to impart flame retardancy while maintaining or improving processing characteristics and other important properties.

Abstract: The invention relates to the use of amino terminated phosphonamides and their oligomers, as flame retardant additives for a variety of polymers to impart flame retardancy while maintaining or improving processing characteristics and other important properties.

Abstract: A tether system for providing thrust to or power subsystems of an artificial satellite in a low earth orbit. The tether has three main sections, an insulated section connected to the satellite, a conducting section connected to the insulating section for drawing in and releasing electrons from the space plasma and a non-conducting section for providing a tension to the other sections of the tether. An oxygen resistant coating is applied to the bare wire of the conducting section as well as the insulated wires of the insulated section that prevents breakdown during tether operations in the space plasma. The insulated and bare wire sections also surround a high tensile flexible polymer core to prevent any debris from breaking the tether during use.