The TF-TJ900C turbojet engine has a rated thrust of 90 kilograms.
The engine has a diameter of 202 mm and a length of 478.5 mm.
The engine has a net weight of 10.45 kg.
The maximum operating altitude for the TF-TJ900C is 11,000 meters.
The ground starting time for the TF-TJ900C engine is less than 50 seconds.
The maximum operating Mach number for the TF-TJ900C is 0.8 Ma.
The TBO for the TF-TJ900C is 20 hours.
The TF-TJ900C engine is suitable for commercial aviation, military aircraft, research and development, training purposes, and specialized missions.
Yes, the TF-TJ900C engine is designed for commercial aviation, including passenger jets.
Yes, the engine is suitable for military aircraft involved in defense operations.
The single gross weight of the TF-TJ900C engine is 3.000 kg.
The single package size for the TF-TJ900C engine is 20 x 20 x 35 cm.
The TF-TJ900C engine is built with robust construction and the latest technology to ensure reliability and long-lasting performance.
The TF-TJ900C engine can be used for training purposes in aviation schools.
Yes, it is suitable for research and development in aerospace engineering.
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