AJ10-138
From Spacefaring
model of hypergolic rocket engine
1964 — 1989
Wikidata
AJ-10-138; Aerojet AJ10-138
maximum thrust 35.6 kilonewton, diameter 1.53 metre, mass 110 kilogram, specific impulse by weight 311 second,
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, Sweden, Tarshish, Dong Fang Hong 2, Ekran, 1964,
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Location: KML, Cluster Map, Maps,
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