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About: TR-107     Goto   Sponge   NotDistinct   Permalink

An Entity of Type : yago:Whole100003553, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)

Type: softwareyago:WikicatRocketEnginesyago:Artifact100021939yago:Device103183080yago:Engine103287733yago:Instrumentality103575240yago:JetEngine103596285yago:Machine103699975yago:Motor103789946yago:Object100002684yago:PhysicalEntity100001930yago:Reaction-propulsionEngine104057435yago:Rocket104099175yago:Whole100003553 New Facet based on Instances of this Class

The TR-107 was a developmental rocket engine designed in 2002 by Northrop Grumman for NASA and DoD funded Space Launch Initiative. Operating on LOX/RP-1 the engine was throttleable and had a thrust of 4,900 kN (1,100,000 lbf) at a chamber pressure of 17.7 megapascals (177 bar), making it one of the most powerful engines ever constructed.