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Using an aerospace engine test stand usually used to precisely test spacecraft engines like ion drives, [17] [56] [57] they reported a maximum thrust of 720 mN at 2,500 W of input power. [57] Yang noted that her results were tentative, and said she "[was] not able to discuss her work until more results are published".
Thrustmaster is an American designer, developer and manufacturer of joysticks, game controllers, and steering wheels for PCs and video gaming consoles. It has licensing agreements with third party brands as Airbus, Boeing, Ferrari, Gran Turismo and U.S. Air Force as well as licensing some products under Sony's PlayStation and Microsoft's Xbox licenses.
Rolls-Royce Tay on a Fokker 100, with thrust reverser engaged. Originally designated 610-8, all but one training engine have now been converted to 611-8 standard. The newest variant is the 611-8C, which has cast HP1 turbine blades, larger fan from the 650-15, structural by-pass duct and FADEC .
The craft developed enough thrust to rise rapidly or to fly horizontally for several minutes. [10] [12] In November 2018 the first self-contained ion-propelled fixed-wing airplane, the MIT EAD Airframe Version 2 flew 60 meters. It was developed by a team of students led by Steven Barrett from the Massachusetts Institute of Technology.
Maximum pressure ratio is increased to 50:1 from 36:1 and it has a bleed air system for environmental control and wing anti-icing. [ 7 ] Compared to the 20-year-older Trent 700 introduced in 1995, the Trent 7000 features a smaller fan hub and a larger fan —112 inches (2.8 m) compared to 97 inches (2.5 m).
Developed by GE Aircraft Engines during the late 1960s, the original engine comprises a single stage fan, driven by a 4-stage low pressure (LP) turbine, supercharging a 14-stage high pressure (HP) compressor, driven by a 2-stage HP turbine.
The latest version of the tri-axial engine, the "-5" and the "-5+" variants are the only tri-axial models still in production. One significant change from the early models to these later ones is the use of an ECU to monitor the performance of the engine and adjust fuel flow accordingly.
It is 33.4 m (110 ft) long and has a 33.6 m (110 ft)-wide, high aspect ratio carbonfibre wing, a first for a Dassault business jet. [1] It is powered by two Rolls-Royce Pearl 10X engines with over 80 kN (18,000 lbf) thrust, with a titanium fan blisk, a 10-stage HP compressor, a two-stage shroudless HP turbine and a four-stage LP turbine. [1]
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