ABCDEFGHIJKLMNOPQRSTUVWXYZ
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Assumed Parameter for an aircraft model as Airbus A310
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Gross Weight [mass] (kg)164000
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Coefficient of Roling Resistance [Urr]0.02
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Air Density [rho] (kg/m^3)1.25
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Drag Coefficient [Cd]0.02685
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Frontal Area [A] (m^2)693.62
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Velocity (m/s)5.56
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Gravitational Force (m/s^2)9.81
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Assumed Parameter for Towing vehicle TBL-280 Mk4
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Gross Weight [mass] (kg)35000
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Coefficient of Roling Resistance [Urr]0.02
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Air Density [rho] (kg/m^3)1.25
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Drag Coefficient [Cd]0.6
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Frontal Area [A] (m^2)6.8
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Velocity (m/s)5.56
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Run Time for Towing Vehice (mins)20
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Gravitational Force (m/s^2)9.81
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Motor Parameters
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Motor TypeREB 90
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Motor Voltage (V)400
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Motor Rating (kW)60
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Working Rotation (rpm)1500
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Max. Torque (N-m)300
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Weight (g)22000
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CoolingAir
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Battery Parameters
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Battery Input Voltage (V)620
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Force Caculation for Aircraft
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Rollling Resistance Force [Frr1] (N)32176.80
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Aerodynamic Drag Force [Fad1] (N)359.83
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Force Calculation for Towing Vehice
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Rollling Resistance Force [Frr2] (N)6867
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Aerodynamic Drag Force [Fad2] (N)78.83
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The Total Force [F] (N)39482.46
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Power required to push/pull the Aircraft [P] (kW)219.52
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Energy Caculation for Towing Vehicle
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Energy [E] (kWh)73.17415573
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Duty Cycle Calculation for Towing Vehice
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Power Input (kW)248
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Duty Cycle 88.52%
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