AJ10-118F
From Spacefaring
model of hypergolic rocket engine
Wikidata
AJ-10-118F; Aerojet AJ10-118F
diameter 1.4 metre, maximum thrust 41.4 kilonewton, specific impulse by weight 306 second, mass 95 kilogram,
Aerojet, United States,
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, 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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