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NASA-LLIS-4618

Lessons Learned - Cryogenic Line Sizing

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 2010

Abstract: A major problem in designing a cryogenic system in a spacecraft or launch vehicle is avoiding back-pressure buildup, which will affect the ability to service and deservice the vehicle with cryogenic reactants. Servicing lines should be sized adequately for an existing baseline system; then the baseline tubing should be oversized to accommodate increased fluid flow rates that can result from new equipment or changes in requirements. If these accommodations are not part of the initial design, servicing or venting paths may need to be added later.
URI: http://yse.yabesh.ir/std;jsery=autho1826ear3081DAC4/handle/yse/190379
Subject: Acquisition / procurement strategy and planning
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    NASA-LLIS-4618

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:07:29Z
date available2017-09-04T18:07:29Z
date copyright09/20/2010
date issued2010
identifier otherGOYEOEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho1826ear3081DAC4/handle/yse/190379
description abstractA major problem in designing a cryogenic system in a spacecraft or launch vehicle is avoiding back-pressure buildup, which will affect the ability to service and deservice the vehicle with cryogenic reactants. Servicing lines should be sized adequately for an existing baseline system; then the baseline tubing should be oversized to accommodate increased fluid flow rates that can result from new equipment or changes in requirements. If these accommodations are not part of the initial design, servicing or venting paths may need to be added later.
languageEnglish
titleNASA-LLIS-4618num
titleLessons Learned - Cryogenic Line Sizingen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2010
contenttypefulltext
subject keywordsAcquisition / procurement strategy and planning
subject keywordsCrew Operations
subject keywordsCrew operations and support concepts
subject keywordsCryogenic Systems
subject keywordsEngineering design and project processes and standards
subject keywordsLaunch Vehicle
subject keywordsLevel II/III requirements definition
subject keywordsLong term sustainability and maintenance planning
subject keywordsMission and systems trade studies
subject keywordsOrbiting Vehicles
subject keywordsPressure Vessels
subject keywordsSpacecraft
subject keywordsSystems analysis - cost analysis
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DSpace software copyright © 2017-2020  DuraSpace
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