AJ10-138
From Spacefaring
Q135224532
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,
United States, Dong Fang Hong 2, Ekran, 1964, liquid propellant rocket engine, 1960s,
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Location: KML, Cluster Map, Maps,
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