Propellant Composition Containing Beryllium and an Energetic Difluoramino Containing Binder.
DEPARTMENT OF THE NAVY WASHINGTON D C
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The patent relates to a high energy composite propellant composition comprising a fuel component of beryllium, beryllium hydride and mixtures thereof in an energic difluoramino containing binder material such as 2,3-bisdifluoraminopropyl acrylate NFPA addition polymerized with a vinyl monomer such as 2-hydroxyl propyl methacrylate and further plasticized with 1,2,3-trisalpha beta-bisdifluoraminoethoxy propane TVOPA, additional oxidizer such as ammonium perchlorate in amount sufficient to assure complete oxidation of the binder and fuel component and cured.
- Solid Rocket Propellants