AJ10-137
From Spacefaring
Q134974783
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,
United States, Dong Fang Hong 2, 1966, liquid propellant rocket engine, 1960s,
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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 | ||
