Payload Weight given Fuel and Empty Weight Fractions Solution

STEP 0: Pre-Calculation Summary
Formula Used
Payload Carried = Desired Takeoff Weight*(1-Empty Weight Fraction-Fuel Fraction)-Crew Weight
PYL = DTW*(1-Ef-Ff)-Wc
This formula uses 5 Variables
Variables Used
Payload Carried - (Measured in Kilogram) - Payload Carried (passengers and cargo) is the object or the entity which is being carried by an aircraft or a launch vehicle.
Desired Takeoff Weight - (Measured in Kilogram) - Desired Takeoff Weight (or mass) is the weight of the aircraft.
Empty Weight Fraction - Empty Weight Fraction is the ratio of the operating empty weight to the desired takeoff weight.
Fuel Fraction - Fuel Fraction is the ratio between weight of fuel caried by a plane to the aircraft total take off weight.
Crew Weight - (Measured in Kilogram) - Crew Weight is the weight of staff which are required for the functioning of the plane. It contains the weight of Pilots, flight engineer, navigation pilot and airplane staff to serve the passengers.
STEP 1: Convert Input(s) to Base Unit
Desired Takeoff Weight: 250000 Kilogram --> 250000 Kilogram No Conversion Required
Empty Weight Fraction: 0.5 --> No Conversion Required
Fuel Fraction: 0.4 --> No Conversion Required
Crew Weight: 12600 Kilogram --> 12600 Kilogram No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
PYL = DTW*(1-Ef-Ff)-Wc --> 250000*(1-0.5-0.4)-12600
Evaluating ... ...
PYL = 12400
STEP 3: Convert Result to Output's Unit
12400 Kilogram --> No Conversion Required
FINAL ANSWER
12400 Kilogram <-- Payload Carried
(Calculation completed in 00.020 seconds)

Credits

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Created by Vedant Chitte
All India Shri Shivaji Memorials Society's ,College of Engineering (AISSMS COE PUNE), Pune
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National Institute Of Technology (NIT), Hamirpur
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Preliminary Design Calculators

Optimum Range for Jet Aircraft in Cruising Phase
​ LaTeX ​ Go Range of Aircraft = (Velocity at Maximum Lift to Drag Ratio*Maximum Lift-to-Drag Ratio of Aircraft)/Power Specific Fuel Consumption*ln(Weight of Aircraft at Beginning of Cruise Phase/Weight of Aircraft at End of Cruise Phase)
Preliminary Take Off Weight Built-up for Manned Aircraft
​ LaTeX ​ Go Desired Takeoff Weight = Payload Carried+Operating Empty Weight+Fuel Weight to be Carried+Crew Weight
Preliminary Take off Weight Built-Up for Manned Aircraft given Fuel and Empty Weight Fraction
​ LaTeX ​ Go Desired Takeoff Weight = (Payload Carried+Crew Weight)/(1-Fuel Fraction-Empty Weight Fraction)
Fuel Fraction
​ LaTeX ​ Go Fuel Fraction = Fuel Weight to be Carried/Desired Takeoff Weight

Payload Weight given Fuel and Empty Weight Fractions Formula

​LaTeX ​Go
Payload Carried = Desired Takeoff Weight*(1-Empty Weight Fraction-Fuel Fraction)-Crew Weight
PYL = DTW*(1-Ef-Ff)-Wc

What is Payload Weight?

Payload is the object or the entity which is being carried by an aircraft or launch vehicle. Sometimes payload also refers to the carrying capacity of an aircraft or launch vehicle, usually measured in terms of weight. Depending on the nature of the flight or mission, the payload of a vehicle may include cargo, passengers, munitions, scientific instruments or experiments, or other equipment. Extra fuel, when optionally carried, is also considered part of the payload. In a commercial context (i.e., an airline or air freight carrier), payload may refer only to revenue-generating cargo or paying passengers. A payload of ordnance carried by a combat aircraft is sometimes alternatively referred to as the aircraft's war load.

How to Calculate Payload Weight given Fuel and Empty Weight Fractions?

Payload Weight given Fuel and Empty Weight Fractions calculator uses Payload Carried = Desired Takeoff Weight*(1-Empty Weight Fraction-Fuel Fraction)-Crew Weight to calculate the Payload Carried, The Payload Weight given Fuel and Empty Weight Fractions formula refers to the total weight of all the items carried by an aircraft, excluding the essential components of the aircraft itself such as the airframe, engines, fuel, and crew, to calculate the payload weight given the fuel and empty weight fractions, you need to subtract the combined weight of the fuel and the empty weight from the total takeoff weight. Payload Carried is denoted by PYL symbol.

How to calculate Payload Weight given Fuel and Empty Weight Fractions using this online calculator? To use this online calculator for Payload Weight given Fuel and Empty Weight Fractions, enter Desired Takeoff Weight (DTW), Empty Weight Fraction (Ef), Fuel Fraction (Ff) & Crew Weight (Wc) and hit the calculate button. Here is how the Payload Weight given Fuel and Empty Weight Fractions calculation can be explained with given input values -> 24820 = 250000*(1-0.5-0.4)-12600.

FAQ

What is Payload Weight given Fuel and Empty Weight Fractions?
The Payload Weight given Fuel and Empty Weight Fractions formula refers to the total weight of all the items carried by an aircraft, excluding the essential components of the aircraft itself such as the airframe, engines, fuel, and crew, to calculate the payload weight given the fuel and empty weight fractions, you need to subtract the combined weight of the fuel and the empty weight from the total takeoff weight and is represented as PYL = DTW*(1-Ef-Ff)-Wc or Payload Carried = Desired Takeoff Weight*(1-Empty Weight Fraction-Fuel Fraction)-Crew Weight. Desired Takeoff Weight (or mass) is the weight of the aircraft, Empty Weight Fraction is the ratio of the operating empty weight to the desired takeoff weight, Fuel Fraction is the ratio between weight of fuel caried by a plane to the aircraft total take off weight & Crew Weight is the weight of staff which are required for the functioning of the plane. It contains the weight of Pilots, flight engineer, navigation pilot and airplane staff to serve the passengers.
How to calculate Payload Weight given Fuel and Empty Weight Fractions?
The Payload Weight given Fuel and Empty Weight Fractions formula refers to the total weight of all the items carried by an aircraft, excluding the essential components of the aircraft itself such as the airframe, engines, fuel, and crew, to calculate the payload weight given the fuel and empty weight fractions, you need to subtract the combined weight of the fuel and the empty weight from the total takeoff weight is calculated using Payload Carried = Desired Takeoff Weight*(1-Empty Weight Fraction-Fuel Fraction)-Crew Weight. To calculate Payload Weight given Fuel and Empty Weight Fractions, you need Desired Takeoff Weight (DTW), Empty Weight Fraction (Ef), Fuel Fraction (Ff) & Crew Weight (Wc). With our tool, you need to enter the respective value for Desired Takeoff Weight, Empty Weight Fraction, Fuel Fraction & Crew Weight and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Payload Carried?
In this formula, Payload Carried uses Desired Takeoff Weight, Empty Weight Fraction, Fuel Fraction & Crew Weight. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Payload Carried = Desired Takeoff Weight-Operating Empty Weight-Crew Weight-Fuel Weight to be Carried
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