Question
A turbojet aircraft is designed to carry a 58,313 lb payload. The Structural Weight fraction is 0.42 and the fuel weight fraction is 0.26.
A turbojet aircraft is designed to carry a 58,313 lb payload. The Structural Weight fraction is 0.42 and the fuel weight fraction is 0.26. Find the gross weight of the aircraft in lb (overall weight) knowing that: thrust -to-weight ratio = 0.30 thrust-to-engine weight ratio = 4.6
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