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The GEnx turbofan engine has a thrust/weight ratio from 5.15-5.62, according to the Wikipedia page https://en.wikipedia.org/wiki/General_Electric_GEnx. As a cautionary note, please consider the operating condition at which the thrust and power are rated. In other words, where was the power rated in the flight envelope (i.e. take-off, climb, cruise, etc)? ...


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