| 摘要 |
The invention relates to a missile structural wall, in particular for a thermal protection fairing. The structural wall (10) of a missile, in particular of a protective fairing (2) of the missile, comprises a structural part (11) provided with an outer surface (12) and an inner surface (13), as well as comprising, at least at a front end of the structural part (11), an outer thermal protection layer (14) on the outer surface (12) and an inner thermal protection layer (15) on the inner surface (13), the inner layer (15) being made from a material having a density that is between 2 and 20 times lower than that of the material of the outer layer (14). |
