A novel and improved EPDM formulation for a solid propellant rocket motor is described wherein hexadiene EPDM monomer components are replaced by alkylidene norbornene components, and, with appropriate adjustment of curing and other additives, functionally required rheological and physical characteristics are achieved with the desired compatibility with any one of a plurality of solid filler materials, e.g., powder silica, carbon fibers or aramid fibers, and with appropriate adhesion and extended storage or shelf-life characteristics.

 
Web www.patentalert.com

< Volume bragg lasers based on high efficiency diffractive elements in photo-thermo-refractive glass

> Self supporting knock-down display frame device having a multitude of interchangeable parts engaged by an integral frame fastening and frame support device

~ 00432