AJ10-137

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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, 
liquid propellant rocket engine, 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, Chinland, Calvinist Republic of Ghent, Ashkenaz, 

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Location: KML, Cluster Map, Maps,


    Apollo 15 CSM Endeavour during rendezvousApollo 15 CSM Endeavour during rendezvous
    Apollo CSM lunar orbitApollo CSM lunar orbit
    Chambre-de-combustion-du-moteur-AJ10-137Chambre-de-combustion-du-moteur-AJ10-137
      TypeSubtypeDateDescriptionNotesSource
      commonsimageApollo 15 CSM Endeavour during rendezvous Commons
      commonsimageApollo CSM lunar orbit Commons
      commonsimageChambre-de-combustion-du-moteur-AJ10-137 Commons
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