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Mission fuel Calculator

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✖Fuel load may be available fuel (consumable fuel) or total fuel and is usually dry weight.ⓘ Fuel load [Wf]
+10%
-10%
✖Reserve fuel for manoeuvring, holding, aborting the landing and making a diversion flight.ⓘ Reserve fuel [Wresf]
+10%
-10%
✖Mission fuel is that fuel at the time of take-off.ⓘ Mission fuel [Wmisf]
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Formula
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Mission fuel

Formula
`"W"_{"misf"} = "W"_{"f"}-"W"_{"resf"}`

Example
`"8085kg"="8823kg"-"738kg"`

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Mission fuel Solution

STEP 0: Pre-Calculation Summary
Formula Used
Mission fuel = Fuel load-Reserve fuel
Wmisf = Wf-Wresf
This formula uses 3 Variables
Variables Used
Mission fuel - (Measured in Kilogram) - Mission fuel is that fuel at the time of take-off.
Fuel load - (Measured in Kilogram) - Fuel load may be available fuel (consumable fuel) or total fuel and is usually dry weight.
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
Fuel load: 8823 Kilogram --> 8823 Kilogram No Conversion Required
Reserve fuel: 738 Kilogram --> 738 Kilogram No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Wmisf = Wf-Wresf --> 8823-738
Evaluating ... ...
Wmisf = 8085
STEP 3: Convert Result to Output's Unit
8085 Kilogram --> No Conversion Required
FINAL ANSWER
8085 Kilogram <-- Mission fuel
(Calculation completed in 00.000 seconds)
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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
Kartikay Pandit has verified this Calculator and 300+ more calculators!

24 Conceptual Design Calculators

Aerofoil Thickness for 4 Digit Series
Go Half Thickness = (Maximum Thickness* ((0.2969*((Position Along the chord)^(0.5)))- (0.1260*Position Along the chord)- (0.3516*((Position Along the chord)^(2)))+ (0.2843*((Position Along the chord)^(3)))- (0.1015*((Position Along the chord)^(4)))))/0.2
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 (%)
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
Maximum take off weight
Go Maximum take off weight = Payload/(1-((Operating empty weight/Desired Takeoff Weight of aircraft)+(Fuel load/Desired Takeoff Weight of aircraft)))
Zero fuel weight given mission fuel, reserve and take off weight
Go Zero fuel weight = Desired Takeoff Weight of aircraft-Mission fuel-Reserve fuel
Take off weight given reserve, mission and zero fuel weight
Go Desired Takeoff Weight of aircraft = Zero fuel weight+Reserve fuel+Mission fuel
Mission fuel given take off, reserve and zero fuel weight
Go Mission fuel = Desired Takeoff Weight of aircraft-Zero fuel weight-Reserve fuel
Operating empty weight from unity equation
Go Operating empty weight = Desired Takeoff Weight of aircraft-(Payload+Fuel load)
Fuel load from unity equation
Go Fuel load = Desired Takeoff Weight of aircraft-(Operating empty weight+Payload)
Take off weight from Unity equation
Go Desired Takeoff Weight of aircraft = Operating empty weight+Payload+Fuel load
Payload weight from Unity equation
Go Payload = Desired Takeoff Weight of aircraft-Operating empty weight-Fuel load
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)
Landing weight given take off weight and mission fuel weight
Go Landing Weight = Desired Takeoff Weight of aircraft-Mission fuel
Range increment of aircraft
Go Range increment of aircraft = Design range-Harmonic range
Useful load
Go Useful weight = Gross weight-Operating empty weight
Payload of aircraft
Go Payload = Zero fuel weight-Operating empty weight
Landing weight given zero fuel weight and reserve fuel weight
Go Landing Weight = Zero fuel weight+Reserve fuel
Zero fuel weight given reserve and landing weight
Go Zero fuel weight = Landing Weight-Reserve fuel
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

Mission fuel Formula

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

what is mission fuel?

mission fuel is also known as trip fuel, this is the fuel required by the airplane to reach its destination.

How to Calculate Mission fuel?

Mission fuel calculator uses Mission fuel = Fuel load-Reserve fuel to calculate the Mission fuel, Mission fuel is the fuel required during take off, the formula is deduction of reserve fuel from fuel load. Mission fuel is denoted by Wmisf symbol.

How to calculate Mission fuel using this online calculator? To use this online calculator for Mission fuel, enter Fuel load (Wf) & Reserve fuel (Wresf) and hit the calculate button. Here is how the Mission fuel calculation can be explained with given input values -> 8085 = 8823-738.

FAQ

What is Mission fuel?
Mission fuel is the fuel required during take off, the formula is deduction of reserve fuel from fuel load and is represented as Wmisf = Wf-Wresf or Mission fuel = Fuel load-Reserve fuel. Fuel load may be available fuel (consumable fuel) or total fuel and is usually dry weight & Reserve fuel for manoeuvring, holding, aborting the landing and making a diversion flight.
How to calculate Mission fuel?
Mission fuel is the fuel required during take off, the formula is deduction of reserve fuel from fuel load is calculated using Mission fuel = Fuel load-Reserve fuel. To calculate Mission fuel, you need Fuel load (Wf) & Reserve fuel (Wresf). With our tool, you need to enter the respective value for Fuel load & Reserve fuel 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 Mission fuel?
In this formula, Mission fuel uses Fuel load & Reserve fuel. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Mission fuel = Desired Takeoff Weight of aircraft-Zero fuel weight-Reserve fuel
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