NASA-LLIS-0759

Lessons Learned – Solid Rocket Motor Joint Reliability

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:50:30Z
date available	2017-09-04T18:50:30Z
date copyright	04/05/2000
date issued	2000
identifier other	KVCEQCAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std/handle/yse/232000
description abstract	Practice: Critical design features that reduce joint rotation, improve seal features, provide close tolerances, provide for leak checks, and provide venting are used to improve the reliability of case-to-case and case-to-nozzle field joints for large solid propellant rocket motors. Principal design drivers are the combustion chamber pressure vs. time profile, segment stacking and assembly tolerances, insulation and sealing configurations, launch dynamic loads, flight dynamic loads, and environmental temperatures.
language	English
title	NASA-LLIS-0759	num
title	Lessons Learned – Solid Rocket Motor Joint Reliability	en
type	standard
page	5
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;2000
contenttype	fulltext