FSI-T225M High Bypass Turbofan Engine:
Specifications:
Maximum Thrust: 225,000 lbf (1000 kN)
Bypass Ratio: 12:1
Overall Bypass Ratio: 76:1
Diameter: 198 inches (5 meters)FSI-T500M High Bypass Contra-Rotating Turbofan Engine:
Specifications:
Maximum Thrust: 500,200 lbf (2225 kN)
Bypass Ratio: 15:1
Overall Bypass Ratio: 120:1
Fan Diameter: 272 inches (6.9 meters)
Engine Diameter: 300 inches (7.6 meters)
Fan Type: Contra-Rotating
Turbine Spools: 4x—
Lore: FSI-T225M
Due to requests by the Combat Aircraft Division (CAD) at FSI for a more powerful yet efficient engine than the GE-9X, the Power-Plant Division (PPD) cooked up the FSI-T225M. A truly massive engine, at the maximum existing proven technology can accomplish.Lore: FSI-T500M
Apparently the T225M isn't enough for CAD's main project at the moment, though to not waste the extensive R&D, found uses for many future and current smaller projects. Also to save on development, the engine core of the T225M was used to develop the T500M. An engine dwarfing even the largest propeller ever made, a hybrid between Turbofan Engines and Contrarotating Turboprops, at the absolute practical size limit for a propeller or fan, while producing as much thrust as possible. Special ducting allows the core's heat to apply the Meredith Effect to the Bypass Air, allowing an even further boost to thrust, at the cost of the air going supersonic inside the engine and exhaust. Suffice to say, but noise level wasn't a concern. In fact, it produces a constant sonic boom in a hemisphere 180 degrees behind the engine, louder than even the XF-84H Banshee. Generating shockwaves powerful enough to knock over small cars on their own. Each jet engine is about 1/3 the thrust of the Saturn 5's F1 Rocket engine and the diameter of the Boeing 777's fuselage.
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