AJ10-118E

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Q135224759




model of hypergolic rocket engine

Wikidata
AJ-10-118E; Aerojet AJ10-118E
mass 90 kilogram, specific impulse by weight 278 second, maximum thrust 35.1 kilonewton, diameter 1.4 metre, 
liquid propellant rocket engine, Aerojet, United States, 
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, Republic of Haiti, liquid propellant rocket engine, 

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Location: KML, Cluster Map, Maps,


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