Antares 2

Antares 2 (X-259) was an American solid rocket engine stage and engine built by Hercules/ABL / Thiokol. It was used from the mid-1960s to 1995, in the Scout and Strypi family of rockets, and on the Project FIRE Velocity Packages. It burned solid propellant – the stage was also the engine's fuel chamber - and was used about 96 times.

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1962 — 1995  Wikimedia, Wikidata
diameter 0.78 metre, mass 1400 kilogram, height 2.9 metre, specific impulse by weight 293 second, maximum thrust 93.1 kilonewton, 
rocket stage, solid-propellant rocket, Thiokol, United States, 
Persia, Republic of Haiti, 1962, Ekran, Dong Fang Hong 2, Tarshish, Sweden, Sikh Confederacy, Reman, United States, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, Ashkenaz, 

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Location: KML, Cluster Map, Maps,

Frameless

EL-2002-00420

Antares X259 rocket stage

Type	Subtype	Date	Description	Notes	Source
commons	image		EL-2002-00420		Commons
commons	image		Antares X259 rocket stage		Commons