R-1E

model of hypergolic rocket engine

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1981  Wikidata
Aerojet R-1E; Marquardt R-1E
mass 2 kilogram, length 31.19 centimetre, specific impulse by weight 280 second, maximum thrust 111 newton, diameter 15.24 centimetre, 
liquid propellant rocket engine, Aerojet Rocketdyne, 
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Sweden, Tarshish, Dong Fang Hong 2, Ekran, 1981, 

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Location: KML, Cluster Map, Maps,

Type	Subtype	Date	Description	Notes	Source