AJ10-118
From Spacefaring
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,
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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