NASA-LLIS-0613

Lessons Learned – Solid Rocket Booster, Bonding Material Process

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:52:08Z
date available	2017-09-04T15:52:08Z
date copyright	04/20/1997
date issued	1997
identifier other	QMCEQCAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/55432
description abstract	Description of Driving Event: To meet environmental requirements, a program decision was made to change the Pressure Sensitive Adhesive used in the J-flap of the segment of the Shuttle Reusable Solid Rocket Motor (RSRM) and the solvent used in the joint cleaning process. A new Pressure Sensitive Adhesive was acquired and a solvent-based cleaning wipe was replaced with an aqueous-based joint cleaning process. Post flight analysis of the RSRM flight article revealed greater than expected erosion, sooting and heat effects on the insulation interfaces.
language	English
title	NASA-LLIS-0613	num
title	Lessons Learned – Solid Rocket Booster, Bonding Material Process	en
type	standard
page	2
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1997
contenttype	fulltext
subject keywords	Environment
subject keywords	Parts Materials & Processes