NASA-LLIS-0689

Lessons Learned – Fiber-Reinforced Polymer Composite Material Selection

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T16:53:15Z
date available	2017-09-04T16:53:15Z
date copyright	03/09/2000
date issued	2000
identifier other	WVCEQCAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/116671
description abstract	Practice: Material selection is an important aspect of design. Often the success of the design is critically dependent on a material or materials performing as desired. This is especially true in the case of advanced composite materials with polymer matrices reinforced with carbon or aramid (Kevlar®) fibers. The important considerations necessary for a proper selection of a fiber-reinforced polymer composite material in NASA spacecraft and satellite structures include fiber material, fiber reinforcement form, fiber volume, matrix material, ply lamination, processing, cost, database, health and safety factors and end-item properties.
language	English
title	NASA-LLIS-0689	num
title	Lessons Learned – Fiber-Reinforced Polymer Composite Material Selection	en
type	standard
page	10
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;2000
contenttype	fulltext