How is Thrust to Weight ratio represented?
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How is Thrust to Weight ratio represented?
Is it just total thrust of 2 engines in lbs over aircraft MTOW in lb
77000 lbs thrust each, so multiply by 2 = 154000
154000 divided by 550000 lbs MTOW = 0.28 ?
is 0.28 how it's represented?
77000 lbs thrust each, so multiply by 2 = 154000
154000 divided by 550000 lbs MTOW = 0.28 ?
is 0.28 how it's represented?
