Q7671209: Difference between revisions
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Q7671209
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Latest revision as of 16:05, 17 February 2025
The TR-107 was a developmental rocket engine designed in 2002 by Northrop Grumman for the NASA and DoD-funded Space Launch Initiative (SLI). 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.
Wikimedia, Wikidata
Northrop Grumman, United States,
United States, Dong Fang Hong 2, Ekran, rocket engine,
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Location: KML, Cluster Map, Maps,
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