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NASA-LLIS-0925

Lessons Learned - KAO (Kuiper Airborne Observatory) Cavity Wall Deflections

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 2001

Abstract: Description of Driving Event:
During the post modification pressure test, the fore and aft cavity walls deflected inward until it reached the full pressure (8.0 psi) deflection value at only 2psi. The test was stopped because of the large deflections present at only 2psi. An investigation was performed to determine the cause of the large deflection at 2psi. It was determined that the contractor had underestimated the cavity wall stiffness by a factor of 4.
URI: https://yse.yabesh.ir/std/handle/yse/127684
Subject: Aircraft
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    NASA-LLIS-0925

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:04:06Z
date available2017-09-04T17:04:06Z
date copyright02/20/2001
date issued2001
identifier otherXYTEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/127684
description abstractDescription of Driving Event:
During the post modification pressure test, the fore and aft cavity walls deflected inward until it reached the full pressure (8.0 psi) deflection value at only 2psi. The test was stopped because of the large deflections present at only 2psi. An investigation was performed to determine the cause of the large deflection at 2psi. It was determined that the contractor had underestimated the cavity wall stiffness by a factor of 4.
languageEnglish
titleNASA-LLIS-0925num
titleLessons Learned - KAO (Kuiper Airborne Observatory) Cavity Wall Deflectionsen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2001
contenttypefulltext
subject keywordsAircraft
subject keywordsComputer-Aided Design/Manufacturing/Engineering
subject keywordsConfiguration Management
subject keywordsCryogenic Systems
subject keywordsFlight Equipment
subject keywordsGround Equipment
subject keywordsPressure Vessels
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