Matches in DBpedia 2015-10 for { ?s ?p "The Bell Aerosystems Company XLR81 (Model 8096) was an American liquid-propellant rocket engine, which was used on the Agena upper stage. It burned UDMH and RFNA fed by a turbopump in a fuel rich gas generator cycle. The turbopump had a single turbine with a gearbox to transmit power to the oxidizer and fuel pumps. The thrust chamber was all aluminum regeneratively cooled by oxidizer flowing through gun-drilled passages in the combustion chamber and throat walls."@en }
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- XLR81 comment "The Bell Aerosystems Company XLR81 (Model 8096) was an American liquid-propellant rocket engine, which was used on the Agena upper stage. It burned UDMH and RFNA fed by a turbopump in a fuel rich gas generator cycle. The turbopump had a single turbine with a gearbox to transmit power to the oxidizer and fuel pumps. The thrust chamber was all aluminum regeneratively cooled by oxidizer flowing through gun-drilled passages in the combustion chamber and throat walls.".