An Airfield Soil Pavement Design Method Based on Rut Depth and Cumulative Fatigue

Table 2

Partial parameters of A-type transport aircraft.

Type	Maximum mass during take-off (kN)	Load distribution coefficient of main landing gear	Single-wheel load of main landing gear (kN)	Tire pressure (MPa)	Area of wheel tread (m^2)	Wheel tread width (m)	Distance between wheel on the same side (S/m)	Width of inner track between left and right main wheel (L/m)
A-type transport aircraft	620	0.95	79	0.78	0.111	0.2764	0.490	4.43