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NASA-LLIS-4596

Lessons Learned - Deaeration of Hydraulic Fluid

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 2011

Abstract: Description of Driving Event:
To meet Space Shuttle launch requirements, the proportion of dissolved air in the Orbiter's hydraulic fluid must be below 1 volume percent. Early in the Shuttle program, the deaeration system that removed the dissolved air from the hydraulic fluid was found to be unreliable and could not meet this requirement. A greater proportion of dissolved air could lead to pump cavitation and excessive softness in hydraulic-actuator force-versus-displacement characteristics.
URI: https://yse.yabesh.ir/std/handle/yse/1720
Subject: Ground processing and manifesting
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    NASA-LLIS-4596

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:04:20Z
date available2017-09-04T15:04:20Z
date copyright06/03/2011
date issued2011
identifier otherKYXKMEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/1720
description abstractDescription of Driving Event:
To meet Space Shuttle launch requirements, the proportion of dissolved air in the Orbiter's hydraulic fluid must be below 1 volume percent. Early in the Shuttle program, the deaeration system that removed the dissolved air from the hydraulic fluid was found to be unreliable and could not meet this requirement. A greater proportion of dissolved air could lead to pump cavitation and excessive softness in hydraulic-actuator force-versus-displacement characteristics.
languageEnglish
titleNASA-LLIS-4596num
titleLessons Learned - Deaeration of Hydraulic Fluiden
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2011
contenttypefulltext
subject keywordsGround processing and manifesting
subject keywordsSystems analysis - cost analysis
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