Fuel Weight to be Carried given Desired Takeoff Weight Solution

STEP 0: Pre-Calculation Summary
Formula Used
Fuel Weight to be carried = Desired Takeoff Weight of Aircraft-Payload Carried-Operating Empty Weight
FW = D-PYL-OEW
This formula uses 4 Variables
Variables Used
Fuel Weight to be carried - (Measured in Tonne) - Fuel Weight to be carried is defined as the total mass of the fuel to be carried (usually includes reserve fuel).
Desired Takeoff Weight of Aircraft - (Measured in Tonne) - Desired Takeoff Weight of Aircraft is the weight of the aircraft.
Payload Carried - (Measured in Tonne) - Payload Carried (passengers and cargo), Payload is the object or the entity which is being carried by an aircraft or a launch vehicle.
Operating Empty Weight - (Measured in Tonne) - Operating Empty Weight of the Aircraft, The empty weight of an aircraft is the weight of the aircraft without including passengers, baggage, or fuel.
STEP 1: Convert Input(s) to Base Unit
Desired Takeoff Weight of Aircraft: 36.1 Tonne --> 36.1 Tonne No Conversion Required
Payload Carried: 25 Tonne --> 25 Tonne No Conversion Required
Operating Empty Weight: 10 Tonne --> 10 Tonne No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
FW = D-PYL-OEW --> 36.1-25-10
Evaluating ... ...
FW = 1.1
STEP 3: Convert Result to Output's Unit
1100 Kilogram -->1.1 Tonne (Check conversion here)
FINAL ANSWER
1.1 Tonne <-- Fuel Weight to be carried
(Calculation completed in 00.004 seconds)

Credits

Created by Mithila Muthamma PA
Coorg Institute of Technology (CIT), Coorg
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Lifting Force given Friction Force due to Rolling Resistance
Go Lifting Force of Aircraft = (((Mass Aircraft*[g]*cos(Angle between Runway and Horizontal Plane))-(Force of Friction/Coefficient of Rolling Friction)))
Vehicle Speed for Lifting Force Provided by Wing Body of Vehicle
Go Vehicle Speed = sqrt((Lifting Force of Aircraft/(0.5*Density Altitude for flying*Aircraft Gross Wing Area*Lift Coefficient)))
Lift Coefficient for Lifting Force Provided by Wing Body of Vehicle
Go Lift Coefficient = Lifting Force of Aircraft/(0.5*Density Altitude for flying*(Vehicle Speed^2)*Aircraft Gross Wing Area)
Lifting Force Provided by Wing Body of Vehicle
Go Lifting Force of Aircraft = 0.5*Density Altitude for flying*Vehicle Speed^2*Aircraft Gross Wing Area*Lift Coefficient
Operating Empty Weight when Desired Take-off Weight is considered
Go Operating Empty Weight = Desired Takeoff Weight of Aircraft-Payload Carried-Fuel Weight to be carried
Payload carried when desired take-off weight is considered
Go Payload Carried = Desired Takeoff Weight of Aircraft-Operating Empty Weight-Fuel Weight to be carried
Fuel Weight to be Carried given Desired Takeoff Weight
Go Fuel Weight to be carried = Desired Takeoff Weight of Aircraft-Payload Carried-Operating Empty Weight
Desired Take off Weight
Go Desired Takeoff Weight of Aircraft = Payload Carried+Operating Empty Weight+Fuel Weight to be carried
True Mach number when true aircraft speed
Go True Mach Number = True Aircraft Speed/Speed of Sound
True Aircraft Speed (Mach number)
Go True Aircraft Speed = Speed of Sound*True Mach Number
Speed of Sound (Mach number)
Go Speed of Sound = True Aircraft Speed/True Mach Number

Fuel Weight to be Carried given Desired Takeoff Weight Formula

Fuel Weight to be carried = Desired Takeoff Weight of Aircraft-Payload Carried-Operating Empty Weight
FW = D-PYL-OEW

What is Maximum Structural Payload Weight ?

Maximum Structural Payload Weight (or mass) is the maximum demonstrated payload to be carried without stressing the aircraft fuselage. Maximum zero fuel weight (or mass) is the sum of the operating empty weight and the maximum structural payload weight.

What is maximum takeoff weight?

The maximum takeoff weight or maximum gross takeoff weight or maximum takeoff mass of an aircraft is the maximum weight at which the pilot is allowed to attempt to take off, due to structural or other limits. The analogous term for rockets is gross lift-off mass.

How to Calculate Fuel Weight to be Carried given Desired Takeoff Weight?

Fuel Weight to be Carried given Desired Takeoff Weight calculator uses Fuel Weight to be carried = Desired Takeoff Weight of Aircraft-Payload Carried-Operating Empty Weight to calculate the Fuel Weight to be carried, Fuel Weight to be Carried given Desired Takeoff Weight is defined as total mass of fuel to be carried (usually includes reserve fuel). Fuel Weight to be carried is denoted by FW symbol.

How to calculate Fuel Weight to be Carried given Desired Takeoff Weight using this online calculator? To use this online calculator for Fuel Weight to be Carried given Desired Takeoff Weight, enter Desired Takeoff Weight of Aircraft (D), Payload Carried (PYL) & Operating Empty Weight (OEW) and hit the calculate button. Here is how the Fuel Weight to be Carried given Desired Takeoff Weight calculation can be explained with given input values -> 0.0011 = 36100-25000-10000.

FAQ

What is Fuel Weight to be Carried given Desired Takeoff Weight?
Fuel Weight to be Carried given Desired Takeoff Weight is defined as total mass of fuel to be carried (usually includes reserve fuel) and is represented as FW = D-PYL-OEW or Fuel Weight to be carried = Desired Takeoff Weight of Aircraft-Payload Carried-Operating Empty Weight. Desired Takeoff Weight of Aircraft is the weight of the aircraft, Payload Carried (passengers and cargo), Payload is the object or the entity which is being carried by an aircraft or a launch vehicle & Operating Empty Weight of the Aircraft, The empty weight of an aircraft is the weight of the aircraft without including passengers, baggage, or fuel.
How to calculate Fuel Weight to be Carried given Desired Takeoff Weight?
Fuel Weight to be Carried given Desired Takeoff Weight is defined as total mass of fuel to be carried (usually includes reserve fuel) is calculated using Fuel Weight to be carried = Desired Takeoff Weight of Aircraft-Payload Carried-Operating Empty Weight. To calculate Fuel Weight to be Carried given Desired Takeoff Weight, you need Desired Takeoff Weight of Aircraft (D), Payload Carried (PYL) & Operating Empty Weight (OEW). With our tool, you need to enter the respective value for Desired Takeoff Weight of Aircraft, Payload Carried & Operating Empty Weight and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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