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, 
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Tarshish, A.M. Isayev Chemical Engineering Design Bureau, Dong Fang Hong 2, Ekran, rocket engine, Republic of Haiti, 

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Location: KML, Cluster Map, Maps,


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