Q17104238: Difference between revisions
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Q17104238
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{{Page|TR-106|Classes|US experimental low-cost hydrolox pintle injector rocket engine}} | {{Page|TR-106|Classes|US experimental low-cost hydrolox pintle injector rocket engine|LPCE; TR106; TRW TR-106; low-cost pintle engine}} | ||
Latest revision as of 12:52, 2 September 2025
The TR-106 or low-cost pintle engine (LCPE) was a developmental rocket engine designed by TRW under the Space Launch Initiative to reduce the cost of launch services and space flight. Operating on LOX/LH2 the engine had a thrust of 2892 kN, or 650,000 pounds, making it one of the most powerful engines ever constructed.
Wikimedia, Wikidata
LPCE; TR106; TRW TR-106; low-cost pintle engine
TRW Inc.,
United States, Dong Fang Hong 2, Ekran, rocket engine,
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Location: KML, Cluster Map, Maps,
SSC TR-106 Rocket Engine under testSSC TR-106 Rocket Engine under test| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | SSC TR-106 Rocket Engine under test | Commons | ||
| commons | image | SSC TR-106 Rocket Engine under test | Commons | ||
