R-1E

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(Redirected from R-1E)
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, 

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Location: KML, Cluster Map, Maps,


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