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

Options

A : empty and payload weight

B : fuel, payload, crew, empty and miscellaneous weight

C : fuel and crew weight

D : only passenger and crew weight

Click to view Correct Answer

Previous || Next

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

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?

Mission leg fuel fraction is defined by ___

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 __

What is the working principle of 'fuel-fraction' method?

Aerodynamic Coefficients more Online Exam Quiz

Air Loads

Airfoil Selection-1

Airfoil Selection-3

Conceptual Design Process

Conceptual Sketch Sizing - Empty-Weight Estimation

Conceptual Sketch Sizing - Fuel-Fraction Estimation-2

Conceptual Sketch Sizing - Takeoff-Weight Buildup

Conceptual Sketch Sizing - Takeoff-Weight Calculation

Configuration Layout - Aerodynamic Considerations-1

Configuration Layout - Aerodynamic Considerations-2