R-1E

From Spacefaring

Revision as of 12:50, 2 September 2025 by John (talk | contribs) (Bot: Automated import of articles)
(diff) ← Older revision | Latest revision (diff) | Newer revision → (diff)

Q135011390




model of hypergolic rocket engine

1981  Wikidata
Aerojet R-1E; Marquardt R-1E
diameter 15.24 centimetre, length 31.19 centimetre, maximum thrust 111 newton, mass 2 kilogram, specific impulse by weight 280 second, 
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, Sikh Confederacy, Tarshish, Dong Fang Hong 2, 1981, Republic of Haiti, liquid propellant rocket engine, 1980s, 

    ​


Location: KML, Cluster Map, Maps,


      TypeSubtypeDateDescriptionNotesSource
      Retrieved from "https://spacefaring.info/index.php?title=Q135011390&oldid=12167"