Home
Download PDF
Order CD-ROM
Order in Print
Home
>
United Facilities Criteria CD 1
>
> Figure 12-23. Rigid pavement thickness design chart for C-5A aircraft (Navy)
Figure 12-22. Rigid pavement thickness design chart for C-141 aircraft (Navy)
Figure 12-24. Chart for determining flexural stress for single-wheel gear (Navy)
Pavement Design for Airfields - index
Page Navigation
223
224
225
226
227
228
229
230
231
232
233
UFC
3-260-02
30
June
2001
Figure
12-23.
Rigid
pavement
thickness
design
chart
for
C-5A
aircraft
(Navy)
12-53