TR-106
US experimental low-cost hydrolox pintle injector rocket engine From Wikipedia, the free encyclopedia
US experimental low-cost hydrolox pintle injector rocket engine From Wikipedia, the free encyclopedia
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.[1]
| |
| Country of origin | United States |
|---|---|
| Manufacturer | TRW |
| Application | low-cost throttleable booster engine |
| Liquid-fuel engine | |
| Propellant | Liquid oxygen / LH2 (liquid hydrogen) |
| Performance | |
| Thrust, sea-level | 2,892 kN (650,000 lbf) |
| Dimensions | |
| Dry mass | 00 kg (0 lb) |
The goal of the development was to produce a large, low-cost, easy-to-manufacture booster engine. The design used a single element coaxial pintle injector, a robust type of injector. It also used ablative cooling of the combustion chamber and nozzle instead of the more costly to manufacture regenerative cooling.[1]
The use of the pintle injector allows the engine thrust to be widely throttleable, as was the case for the lunar module descent engine.[1]
Tom Mueller was a lead engineer for development of the LCPE,[2][3] a 650,000 lbf thrust LOX/LH2 engine. In the summer of 2000, this LCPE was successfully hot fire tested at 100 percent of its rated thrust as well as at a 65 percent throttle condition at NASA's John C. Stennis Space Center in Mississippi.[4] TRW changed the pintle injector configuration three times during testing to explore the engine's performance envelope; engineers also replaced the ablative chamber once while the engine was on the test stand—demonstrating the LCPE's ease of operation. Test results demonstrated that the engine was stable over a wide variety of thrust levels and propellant ratios.[1]
Development of the engine was temporarily discontinued with the cancellation of the Space Launch Initiative.[1] In 2002 TRW was acquired by Northrop Grumman and development of a LOX/RP-1 engine (TR-107) continued, under contract to NASA, for potential use on next-generation launch and space transportation vehicles.[5]
Tom Mueller became TRW vice president of propulsion. In 2002, Elon Musk asked Mueller to join him as a founding member of SpaceX.
Technology lessons from the Low Cost Pintle Engine project were used in the development of the SpaceX Merlin engine.[6][7] Mueller joined SpaceX in 2002, becoming its head of propulsion, along with other TRW staffers.[8] The turbopump, meanwhile, was contracted to Barber-Nichols, Inc., which derived their pump from their work on the FASTRAC turbopump.[9] After SpaceX accused Northrop Grumman, TRW's parent, of letting engineers supervising SpaceX under a Pentagon contract use that information on Northrop's own rocket technology, Northrop Grumman then sued for theft of trade secrets.[10][11] The dueling suits were settled in early 2005.[12]
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