Question: Mission leg fuel fraction is defined by ___

Options

A : weight at end of the phase to that of at the begin

B : weight at end of the phase to that of at the begin

C : weight of phase at the begin

D : weight at end of the phase

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Conceptual Sketch Sizing - Fuel-Fraction Estimation-1 more questions

Design take-off gross weight includes __

Determine the corrections or otherwise of the following assertion [A]....

Determine the corrections or otherwise of the following Assertion [A]....

In A/C, we provide reserve fuel for ___

Is it mandatory for Aircraft to carry reserved fuel?

Take-off gross weight of an aircraft is summation of ___

The ?Design take-off gross weight? and ?maximum take-off weight? are....

The subsequent step after the requirements in conceptual design phase....

The typical method for determining fuel weight used is called....

Total fuel weight of aircraft is __

Aerodynamic Coefficients more Online Exam Quiz

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Airfoil Selection-3

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Configuration Layout - Aerodynamic Considerations-2