Accession Number : ADD011360

Title :   Carbon/Carbon Rocket Motor Exit Cone Reinforcement.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON DC

Personal Author(s) : O'Driscoll,P F ; Crowe,G E ; Berry,J

Report Date : 16 Oct 1984

Pagination or Media Count : 4

Abstract : A carbon-carbon rocket motor exit cone having a threaded cylindrical section for attachment to the motor section is reinforced with a plurality of windings of carbon fiber around the cylindrical section. (Author)

Descriptors :   *PATENTS, *EXHAUST NOZZLES, *CONICAL NOZZLES, *SOLID PROPELLANT ROCKET ENGINES, *CARBON CARBON COMPOSITES, EXITS, ROCKET NOZZLES, COMPOSITE STRUCTURES, FIBER REINFORCEMENT, CYLINDRICAL BODIES, FILAMENT WOUND CONSTRUCTION

Subject Categories : Laminates and Composite Materials
      Solid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE