NASA-LLIS-0669

Lessons Learned – Structural Laminate Composites for Space Applications

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:39:43Z
date available	2017-09-04T18:39:43Z
date copyright	03/07/2000
date issued	2000
identifier other	ALCEQCAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;query=authoCA5893FD081D49A96159DD6EFDEC014A/handle/yse/221374
description abstract	Practice: The creation of reliable structural laminate composites for space applications requires precision design and manufacturing using an integrated, concurrent engineering approach. Since the final material characteristics are established at the same time the part or subassembly is fabricated, part design, fabrication development, and material characterization must proceed concurrently. Because composite materials are custom-tailored to meet structural requirements of the assembly, stringent inprocess controls are required to arrive at a configuration with optimum physical and material properties.
language	English
title	NASA-LLIS-0669	num
title	Lessons Learned – Structural Laminate Composites for Space Applications	en
type	standard
page	8
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;2000
contenttype	fulltext