Fuel load Solution

STEP 0: Pre-Calculation Summary
Formula Used
Fuel load = Mission fuel+Reserve fuel
Wf = Wmisf+Wresf
This formula uses 3 Variables
Variables Used
Fuel load - (Measured in Kilogram) - Fuel load may be available fuel (consumable fuel) or total fuel and is usually dry weight.
Mission fuel - (Measured in Kilogram) - Mission fuel is that fuel at the time of take-off.
Reserve fuel - (Measured in Kilogram) - Reserve fuel for manoeuvring, holding, aborting the landing and making a diversion flight.
STEP 1: Convert Input(s) to Base Unit
Mission fuel: 8761 Kilogram --> 8761 Kilogram No Conversion Required
Reserve fuel: 738 Kilogram --> 738 Kilogram No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Wf = Wmisf+Wresf --> 8761+738
Evaluating ... ...
Wf = 9499
STEP 3: Convert Result to Output's Unit
9499 Kilogram --> No Conversion Required
FINAL ANSWER
9499 Kilogram <-- Fuel load
(Calculation completed in 00.016 seconds)

Credits

Created by Himanshu Sharma
National Institute of Technology, Hamirpur (NITH), Himachal Pradesh
Himanshu Sharma has created this Calculator and 50+ more calculators!
Verified by Kartikay Pandit
National Institute Of Technology (NIT), Hamirpur
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19 Design Process Calculators

Summations of priorities of objectives that need to be maximized (Millitary planes)
Go Priority Sum of objectives to be maximized (%) = Performance Priority (%)+Flight Quality Priority (%)+Scariness Priority (%)+Maintainability Priority (%)+Producibility Priority (%)+Disposability Priority (%)+Stealth Priority (%)
Thrust-to-Weight ratio given vertical velocity
Go Thrust-to-weight ratio = ((Vertical Airspeed/Aircraft Velocity)+((Dynamic Pressure/Wing Loading)*(Minimum Drag Coefficient))+((Lift Induced Drag Constant/Dynamic Pressure)*(Wing Loading)))
Priority of objective weight in design process given minimum design index
Go Weight Priority (%) = ((Minimum Design Index*100)-(Cost Index*Cost Priority (%))-(Period Index*Period Priority (%)))/Weight Index
Priority of objective cost in design process given minimum design index
Go Cost Priority (%) = ((Minimum Design Index*100)-(Weight Index*Weight Priority (%))-(Period Index*Period Priority (%)))/Cost Index
Priority of objective period of design given minimum design index
Go Period Priority (%) = ((Minimum Design Index*100)-(Weight Index*Weight Priority (%))-(Cost Index*Cost Priority (%)))/Period Index
Period of Design Index given Minimum Design Index
Go Period Index = ((Minimum Design Index*100)-(Weight Index*Weight Priority (%))-(Cost Index*Cost Priority (%)))/Period Priority (%)
Weight Index given Minimum Design Index
Go Weight Index = ((Minimum Design Index*100)-(Cost Index*Cost Priority (%))-(Period Index*Period Priority (%)))/Weight Priority (%)
Cost Index given Minimum Design Index
Go Cost Index = ((Minimum Design Index*100)-(Weight Index*Weight Priority (%))-(Period Index*Period Priority (%)))/Cost Priority (%)
Minimum design index
Go Minimum Design Index = ((Cost Index*Cost Priority (%))+(Weight Index*Weight Priority (%))+(Period Index*Period Priority (%)))/100
Battery Weight Fraction
Go Battery Weight Fraction = (Range of Aircraft/(Battery Specific Energy Capacity*3600*Efficiency*(1/[g])*Maximum Lift to Drag ratio of Aircraft))
Summation of priorities of all objectives that need to be minimized
Go Priority Sum of objectives to be minimized(%) = Cost Priority (%)+Weight Priority (%)+Period Priority (%)
Electric Power for Wind Turbine
Go Electric Power of Wind Turbine = Shaft Power*Efficiency of Generator*Efficiency of Transmission
Propulsion Net Thrust
Go Thrust force = Air Mass Flow Rate*(Velocity of Jet-Flight Velocity)
Maximum payload capability
Go Payload = Maximum take off weight-Operating empty weight-Fuel load
Induced Inflow Ratio in Hover
Go Inflow Ratio = Induced Velocity/(Rotor Radius*Angular Velocity)
Range increment of aircraft
Go Range increment of aircraft = Design range-Harmonic range
Mission fuel
Go Mission fuel = Fuel load-Reserve fuel
Reserve fuel
Go Reserve fuel = Fuel load-Mission fuel
Fuel load
Go Fuel load = Mission fuel+Reserve fuel

Fuel load Formula

Fuel load = Mission fuel+Reserve fuel
Wf = Wmisf+Wresf

what is fuel load?

fuel load is considered a total of fuel required during take off and during time of flight and manoeuvring,aborting etc

How to Calculate Fuel load?

Fuel load calculator uses Fuel load = Mission fuel+Reserve fuel to calculate the Fuel load, Fuel load is the amount of fuel present expressed quantitatively in terms of weight of fuel per unit area. This may be available fuel (consumable fuel) or total fuel and is usually dry weight.the formula for calculating fuel load for a specific flight typically involves estimating fuel consumption rates for each phase of the flight and adding reserves for contingencies. Fuel load is denoted by Wf symbol.

How to calculate Fuel load using this online calculator? To use this online calculator for Fuel load, enter Mission fuel (Wmisf) & Reserve fuel (Wresf) and hit the calculate button. Here is how the Fuel load calculation can be explained with given input values -> 9499 = 8761+738.

FAQ

What is Fuel load?
Fuel load is the amount of fuel present expressed quantitatively in terms of weight of fuel per unit area. This may be available fuel (consumable fuel) or total fuel and is usually dry weight.the formula for calculating fuel load for a specific flight typically involves estimating fuel consumption rates for each phase of the flight and adding reserves for contingencies and is represented as Wf = Wmisf+Wresf or Fuel load = Mission fuel+Reserve fuel. Mission fuel is that fuel at the time of take-off & Reserve fuel for manoeuvring, holding, aborting the landing and making a diversion flight.
How to calculate Fuel load?
Fuel load is the amount of fuel present expressed quantitatively in terms of weight of fuel per unit area. This may be available fuel (consumable fuel) or total fuel and is usually dry weight.the formula for calculating fuel load for a specific flight typically involves estimating fuel consumption rates for each phase of the flight and adding reserves for contingencies is calculated using Fuel load = Mission fuel+Reserve fuel. To calculate Fuel load, you need Mission fuel (Wmisf) & Reserve fuel (Wresf). With our tool, you need to enter the respective value for Mission fuel & Reserve fuel 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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