درباره ما
MIL-W-81752A
WINDSHIELD SYSTEMS, FIXED WING AIRCRAFT GENERAL SPECIFICATION FOR
| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T15:40:39Z | |
| date available | 2017-09-04T15:40:39Z | |
| date copyright | 02/27/1987 | |
| date issued | 1987 | |
| identifier other | BAGPDAAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/42845 | |
| description abstract | This specification establishes the general requirements for the design, performance, installation, and acceptance of windshield systems in fixed wing aircraft. Intended Use: The requirements of this specification are intended for use in designing windshield systems for fixed wing aircraft. The windshield system shall provide clear vision for the pilot(s) and provide protection from environmental and other threats. These requirements apply to the transparency materials, framing, support structure, attachments, and seals. | |
| language | English | |
| title | MIL-W-81752A | num |
| title | WINDSHIELD SYSTEMS, FIXED WING AIRCRAFT GENERAL SPECIFICATION FOR | en |
| type | standard | |
| page | 22 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;1987 | |
| contenttype | fulltext | |
| subject keywords | Anti-static coating | |
| subject keywords | Binocular disparity | |
| subject keywords | Fighter/attack type aircraft | |
| subject keywords | Fixed wing aircraft | |
| subject keywords | Optics | |
| subject keywords | Windshield systems |
