R-1E

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Q135011390




model of hypergolic rocket engine

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, 
Sikh Confederacy, 1980s, liquid propellant rocket engine, Republic of Haiti, 1981, Ekran, Dong Fang Hong 2, Tarshish, Sweden, United States, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, Ashkenaz, 

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Location: KML, Cluster Map, Maps,


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