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NASA-LLIS-0127

Lessons Learned - Orbiter Protection System "Y" Curtain Wall Retraction

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1992

Abstract: Description of Driving Event:
During the retraction of the orbiter protection system "Y" curtain wall in the console mode, the speed attained after leaving the slow travel transition is excessive. The operator must manipulate a manual valve to reduce air flow to the winch. High impact stops from the rapid movement of the "Y" curtain wall during retraction may cause personnel injury and/or damage to payloads and facility (PAD).
URI: http://yse.yabesh.ir/std/handle/yse/145611
Subject: Facilities
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  • NASA - National Aeronautics and Space Administration (NASA)
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    NASA-LLIS-0127

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:22:26Z
date available2017-09-04T17:22:26Z
date copyright08/25/1992
date issued1992
identifier otherZVYCQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/145611
description abstractDescription of Driving Event:
During the retraction of the orbiter protection system "Y" curtain wall in the console mode, the speed attained after leaving the slow travel transition is excessive. The operator must manipulate a manual valve to reduce air flow to the winch. High impact stops from the rapid movement of the "Y" curtain wall during retraction may cause personnel injury and/or damage to payloads and facility (PAD).
languageEnglish
titleNASA-LLIS-0127num
titleLessons Learned - Orbiter Protection System "Y" Curtain Wall Retractionen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1992
contenttypefulltext
subject keywordsFacilities
subject keywordsGround Equipment
subject keywordsGround Operations
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