AJ10-118

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Q135224757




model of hypergolic rocket engine

Wikidata
AJ-10-118; Aerojet AJ10-118; Aerojet LR52-AJ-1; LR52-AJ-1
diameter 0.84 metre, specific impulse by weight 271 second, maximum thrust 33.8 kilonewton, mass 90 kilogram, 
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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