MIL-PRF-47257F

COMPOUND, EPOXY, FILAMENT WINDING

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;query=autho47037D83FCDCAC426159DD6EFDEC014A/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