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 00.004 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
Kartikay Pandit has verified this Calculator and 400+ more calculators!

19 Design Process Calculators

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)))
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 (%)
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

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.
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