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,
Aerojet, United States,
Reman, 1960s, liquid propellant rocket engine, Republic of Haiti, 1966, 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,
Apollo 15 CSM Endeavour during rendezvous
Apollo CSM lunar orbit
Chambre-de-combustion-du-moteur-AJ10-137| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | Apollo 15 CSM Endeavour during rendezvous | Commons | ||
| commons | image | Apollo CSM lunar orbit | Commons | ||
| commons | image | Chambre-de-combustion-du-moteur-AJ10-137 | Commons | ||
