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... 14, the total cost of their research and development on the Kavli GTX-35VS project has reached 3.3 billion U.S. dollars. This research funding is much more than ours."
"Hey, the thrust-to-weight ratio is 7.47. This still adds an afterburner, which is not as high as our civil aviation engine. Their engine can only be regarded as the second generation. The fan of the engine is a 3-stage axial flow type and adopts a transonic design. The axial flow type is correct, but if the basic skills ar ...
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