Accession Number : ADD016458

Title :   Solid Fuel Ramjet Composition.

Descriptive Note : Patent, Filed 25 Nov 81, patented 14 Jun 94,

Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON DC

Personal Author(s) : Burdette, George W ; Meyers, Gary W

Report Date : 14 Jun 1994

Pagination or Media Count : 3

Abstract : A ramjet solid fuel composed of Hydroxyl terminated polybutadiene aluminum, magnesium, and boron carbide is described. The high volumetric heating value fuel of the present invention significantly increases the distance range of missiles.

Descriptors :   *SOLID FUELS, *PATENTS, *RAMJET ENGINES, *CHEMICAL COMPOSITION, *HYDROXY TERMINATED POLYBUTADIENE, ALUMINUM, BORON CARBIDES, HEATING, MAGNESIUM, POLYBUTADIENE, GUIDED MISSILES, HYDROXYL RADICALS, LONG RANGE(DISTANCE)

Subject Categories : Fuels
      Guided Missiles
      Inorganic Chemistry
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE