AJ10-137
From Spacefaring
model of hypergolic rocket engine
1966 — 1975
Wikimedia, Wikidata
AJ-10-137; Aerojet AJ10-137; Apollo SPS engine; Apollo Service Propulsion System engine
specific impulse by weight 314.5 second, maximum thrust 91.19 kilonewton,
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, 1966,
Location: KML, Cluster Map, Maps,
Apollo 15 CSM Endeavour during rendezvous
Apollo CSM lunar orbit
Chambre-de-combustion-du-moteur-AJ10-137