AJ10-138
From Spacefaring
model of hypergolic rocket engine
1964 — 1989
Wikidata
AJ-10-138; Aerojet AJ10-138
specific impulse by weight 311 second, maximum thrust 35.6 kilonewton, diameter 1.53 metre, mass 110 kilogram,
Aerojet, United States,
Reman, 1960s, liquid propellant rocket engine, Republic of Haiti, 1964, Ekran, Dong Fang Hong 2, Tarshish, Sikh Confederacy, United States, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, Ashkenaz,
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Location: KML, Cluster Map, Maps,
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