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Rocket Motor, Solid Fuel, X-259

Display Status:
This object is not on display at the National Air and Space Museum, it is either on loan or in storage.

Rocket Motor, Solid Fuel, X-259

 

  • Summary

Manufacturer:   Alleghany Ballistics Laboratory, Hercules Incorporated

Date: ca. 1968

Country of Origin: United States of America

Dimensions:
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)

Materials:
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.

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


Inventory number: A19680240000