Is a single shaft turbojet engine , which consists of 3 stage axial compressor , direct annular combustion chamber and 1 stage axial turbine. This engine has a simple design ,Low cost and high thrust to weight ratio. The speed control of the engine is hydro-pneumatic. The life time of the engine is 20 hr or 50 starts.
Catalog
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chapter 6-11(126)_385_0.pdf | 246.25 KB |
No.
385