NASA-LLIS-0957

Lessons Learned – Solid Rocket Motor Nozzle Internal Seals: Dual "O" Ring Seals and Leak Check Ports

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T16:07:58Z
date available	2017-09-04T16:07:58Z
date copyright	03/27/1995
date issued	1995
identifier other	SCUEQCAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/71186
description abstract	Description of Driving Event: The Challenger (Space Shuttle Flight #51L) accident triggered a detailed review of all of the joints in the Solid Rocket Motor. Analyses showed a potential weakness and potential flow paths for hot gasses through the case-to-nozzle joint that could cause a catastrophic event similar to that encountered in Challenger.
language	English
title	NASA-LLIS-0957	num
title	Lessons Learned – Solid Rocket Motor Nozzle Internal Seals: Dual "O" Ring Seals and Leak Check Ports	en
type	standard
page	2
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1995
contenttype	fulltext
subject keywords	Energetic Materials - Explosive/Propellant/Pyrotechnic
subject keywords	Launch Vehicle