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NASA-LLIS-6116

Lessons Learned - Environment Control and Life Support System (ECLSS) Ground Coolant System (GCS)

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:09:41Z
date available2017-09-04T16:09:41Z
date copyright40851
date issued2011
identifier otherSHLHOEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/72927
description abstractThe basic S70-0508 Ground Coolant Unit design (heat load capacity) was oversized and could not handle the wide range of heat loads required when the Space Shuttle Orbiter is powered up. Electrical modifications were designed that almost completely redesigned the circulation unit. The Universal Coolant Transporter System (UCTS) was designed and delivered. It is important to conduct thorough processes when identifying core requirements for the design, provide a process for continuous improvement recommendations, document work processes, and be persistent in pursuing funding for operationally beneficial design changes.
languageEnglish
titleNASA-LLIS-6116num
titleLessons Learned - Environment Control and Life Support System (ECLSS) Ground Coolant System (GCS)en
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2011
contenttypefulltext
subject keywordsAdditional Categories.Ground Equipment
subject keywordsAdditional Categories.Ground Operations
subject keywordsEngineering Design (Phase C/D).Environmental Control and Life Support Systems
subject keywordsEngineering Design (Phase C/D).Launch Systems
subject keywordsMission Operations and Ground Support Systems.Ground support systems
subject keywordsMission Operations and Ground Support Systems.Launch support systems
subject keywordsSystems Engineering and Analysis.Engineering design and project processes and standards


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