Rocket Motor, Solid Fuel, X-259
This is the X-259, or Antares II, the third-stage, solid-fuel rocket motor for the all-solid fuel U.S. Scout launch vehicle. Antares II produced about 23,500 pounds of thrust. Like the other stages of the Scout, Antares was named after a star constellation. (The Scout's first, second, and fourth stages were the Algol, Castor, and Altair, respectively.)
The Scout was conceived in 1958 as a low-cost launch vehicle for light payloads. The first Scout was launched in 1960 and continued as a very successful vehicle. This object was donated to the Smithsonian in 1968 by the Alleghany Ballistic Laboratory.
Gift of Alleghany Ballistics Laboratory
- Country of Origin
- United States of America
- ca. 1968
- PROPULSION-Rocket Engines
- Filament-wound, resin-bonded glass fiber body with asbestos-filled SBR rubber. Windings by circumferential wraps of glass fiber coated with catalyzed epoxy resin. Aluminum nozzle fixture rings. Aluminum skirt rings bolted underneath forward dome.
- Overall: 2 ft. 4 in. wide x 9 ft. 6 1/2 in. long x 2 ft. 5 in. diameter, 200 lb. (71.12 x 290.83 x 73.66cm, 90.7kg)