Matches in DBpedia 2016-04 for { ?s ?p "RD-270 (Russian: Ра́кетный дв́игатель 270, Rocket Engine 270, 8D420) is a single chamber liquid bipropellant rocket engine designed by Energomash (USSR/Russia) in 1960–1970. It was to be used on the first stages of proposed heavy-lift UR-700 and UR-900 rocket families. It has the highest thrust among single chambered engines of USSR and Russia, 640 metric tons at the surface of Earth. The propellants used are unsymmetrical dimethylhydrazine (UDMH) and nitrogen tetroxide (N2O4)."@en }
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- RD-270 comment "RD-270 (Russian: Ра́кетный дв́игатель 270, Rocket Engine 270, 8D420) is a single chamber liquid bipropellant rocket engine designed by Energomash (USSR/Russia) in 1960–1970. It was to be used on the first stages of proposed heavy-lift UR-700 and UR-900 rocket families. It has the highest thrust among single chambered engines of USSR and Russia, 640 metric tons at the surface of Earth. The propellants used are unsymmetrical dimethylhydrazine (UDMH) and nitrogen tetroxide (N2O4).".
- Q4386506 comment "RD-270 (Russian: Ра́кетный дв́игатель 270, Rocket Engine 270, 8D420) is a single chamber liquid bipropellant rocket engine designed by Energomash (USSR/Russia) in 1960–1970. It was to be used on the first stages of proposed heavy-lift UR-700 and UR-900 rocket families. It has the highest thrust among single chambered engines of USSR and Russia, 640 metric tons at the surface of Earth. The propellants used are unsymmetrical dimethylhydrazine (UDMH) and nitrogen tetroxide (N2O4).".