Dante80
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Because after a certain point, T/W becomes irrelevant. Let's review T/W or the thrust to weight ratio. It is a measure of how quickly an aircraft will accelerate upwards when it acts like a dead weight. Is that how aircrafts behave during combat? The max climb rate needs to factor in the lift to drag ratio. You can get a feel for it from open source videos. Thunder is no slouch in climb rate.
Ok, many thanks for the input..I'm out. C: