Missile structural wall for thermal protection fairing
US9891031B2 · kind B2 · utility
2Cited by
10References
20Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Jun 10, 2015 |
| Grant date | Feb 13, 2018 |
| Priority date | — |
| Expiry date | Jun 10, 2035 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF42B10/46
- WIPO fieldOther special machines
- WIPO sectorMechanical engineering
Abstract
The invention relates to a missile structural wall, in particular for a thermal protection fairing. The structural wall of a missile, in particular of a protective fairing of the missile, comprises a structural part provided with an outer surface and an inner surface, as well as comprising, at least at a front end of the structural part, an outer thermal protection layer on the outer surface and an inner thermal protection layer on the inner surface, the inner layer 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.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.