درباره ما
MIL-STD-1290A
LIGHT FIXED AND ROTARY-WING AIRCRAFT CRASH RESISTANCE
| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T15:25:40Z | |
| date available | 2017-09-04T15:25:40Z | |
| date copyright | 09/26/1988 | |
| date issued | 1988 | |
| identifier other | NLYPDAAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/26284 | |
| description abstract | Purpose. This document establishes minimum crash resistance criteria for implementation in the initial stages of aircraft system design. Classification. The requirements of this specification pertain to the following aircraft types: Type I - Light Fixed-Wing Type II - Rotary-wing, including Tilt Prop/Rotor Aircraft | |
| language | English | |
| title | MIL-STD-1290A | num |
| title | LIGHT FIXED AND ROTARY-WING AIRCRAFT CRASH RESISTANCE | en |
| type | standard | |
| page | 46 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;1988 | |
| contenttype | fulltext | |
| subject keywords | Crash resistance | |
| subject keywords | aircraft | |
| subject keywords | design for | |
| subject keywords | Crash resistance | |
| subject keywords | fixed wing | |
| subject keywords | light aircraft | |
| subject keywords | Crash resistance | |
| subject keywords | rotary-wing aircraft |
