STAR 31

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Q115871251




American solid rocket motor and stage developed by Thiokol

1973  Wikidata
diameter 0.7645 metre, specific impulse by weight 294 second, maximum thrust 80 kilonewton, mass 1384 kilogram, 
rocket stage, STAR, United States, 
United States, Dong Fang Hong 2, Ekran, STAR, 1973, 1970s, 

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Location: KML, Cluster Map, Maps,


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