11D430

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Q12379757




model of Soviet rocket engine

Wikidata
specific impulse by weight 307 second, maximum thrust 29.43 kilonewton, 
rocket engine, A.M. Isayev Chemical Engineering Design Bureau, Soviet Union, 
Reman, Republic of Haiti, rocket engine, Ekran, Dong Fang Hong 2, A.M. Isayev Chemical Engineering Design Bureau, Tarshish, Sweden, Sikh Confederacy, Ashkenaz, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, 

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Location: KML, Cluster Map, Maps,


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