AJ10-220

From Spacefaring

Revision as of 12:42, 2 September 2025 by John (talk | contribs) (Bot: Automated import of articles)
(diff) ← Older revision | Latest revision (diff) | Newer revision → (diff)

Q135011331




model of hypergolic rocket engine

Wikidata
AJ-10-220; Aerojet AJ10-220
maximum thrust 62.3 newton, specific impulse by weight 285 second, diameter 7.3 centimetre, length 19 centimetre, mass 1.95 kilogram, 
liquid propellant rocket engine, Aerojet Rocketdyne, United States, 
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, Republic of Haiti, liquid propellant rocket engine, 

    ​


Location: KML, Cluster Map, Maps,


      TypeSubtypeDateDescriptionNotesSource
      Retrieved from "https://spacefaring.info/index.php?title=Q135011331&oldid=11696"