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MIL-PRF-47257F
COMPOUND, EPOXY, FILAMENT WINDING
Organization:
ARMY - MI - Aviation & Missile Command
Year: 2010
Abstract: This specification covers a fiberglass roving impregnated with an epoxy resin-hardener compound used in the fabrication of filament wound structures.Intended Use: This material is intended for use as an impregnant for fiberglass filaments used in missile systems. The cured parts are satisfactory for use at temperatures from -54 to 121 °C.
Subject: Amine promoter
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| contributor author | ARMY - MI - Aviation & Missile Command | |
| date accessioned | 2017-09-04T18:14:25Z | |
| date available | 2017-09-04T18:14:25Z | |
| date copyright | 07/12/2010 | |
| date issued | 2010 | |
| identifier other | HHLVTCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsein/handle/yse/197338 | |
| description abstract | This specification covers a fiberglass roving impregnated with an epoxy resin-hardener compound used in the fabrication of filament wound structures.Intended Use: This material is intended for use as an impregnant for fiberglass filaments used in missile systems. The cured parts are satisfactory for use at temperatures from -54 to 121 °C. | |
| language | English | |
| title | MIL-PRF-47257F | num |
| title | COMPOUND, EPOXY, FILAMENT WINDING | en |
| type | standard | |
| page | 13 | |
| status | Active | |
| tree | ARMY - MI - Aviation & Missile Command:;2010 | |
| contenttype | fulltext | |
| subject keywords | Amine promoter | |
| subject keywords | Anhydride hardener | |
| subject keywords | Resin-hardener |