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NASA-LLIS-0007

Lessons Learned - Debonding of a Mounting Device (Shuttle Orbiter TV Monitor Bracket) due to Growth of a Pressurized Vessel such as the Crew Cabin Wall Following Launch

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1991

Abstract: Description of Driving Event:
During two successive missions of the shuttle orbiter OV-99, a television monitor secured by a bracket that was bonded to the wall of the crew module, became detached from the wall (debonded). Following the first incident, it was assumed that an improper bonding technique was the cause of the failure. Remounting was accomplished under close surveillance by quality inspectors. Following the second incident, it was concluded that growth of the structural skin of the wall due to pressurization during flight caused the failure. It was explained that this did not occur on orbiter OV-102 because its wall is thicker and subject to less growth from pressurization. An object as large as a TV monitor detaching from its mount during any phase of a mission could become a hazard to personnel or equipment. The wall section of OV-99 used for mounting the monitor was stiffened with wall doublers to reduce growth from pressurization during launch.
URI: https://yse.yabesh.ir/std/handle/yse/80161
Subject: Flight Equipment
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  • NASA - National Aeronautics and Space Administration (NASA)
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    NASA-LLIS-0007

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:16:48Z
date available2017-09-04T16:16:48Z
date copyright04/29/1991
date issued1991
identifier otherTAYCQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/80161
description abstractDescription of Driving Event:
During two successive missions of the shuttle orbiter OV-99, a television monitor secured by a bracket that was bonded to the wall of the crew module, became detached from the wall (debonded). Following the first incident, it was assumed that an improper bonding technique was the cause of the failure. Remounting was accomplished under close surveillance by quality inspectors. Following the second incident, it was concluded that growth of the structural skin of the wall due to pressurization during flight caused the failure. It was explained that this did not occur on orbiter OV-102 because its wall is thicker and subject to less growth from pressurization. An object as large as a TV monitor detaching from its mount during any phase of a mission could become a hazard to personnel or equipment. The wall section of OV-99 used for mounting the monitor was stiffened with wall doublers to reduce growth from pressurization during launch.
languageEnglish
titleNASA-LLIS-0007num
titleLessons Learned - Debonding of a Mounting Device (Shuttle Orbiter TV Monitor Bracket) due to Growth of a Pressurized Vessel such as the Crew Cabin Wall Following Launchen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1991
contenttypefulltext
subject keywordsFlight Equipment
subject keywordsFlight Operations
subject keywordsHardware
subject keywordsLaunch Vehicle
subject keywordsParts Materials & Processes
subject keywordsPressure Vessels
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