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Lessons Learned - Extension of Orbiter Access Arm (OAA)

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:43:37Z
date available2017-09-04T17:43:37Z
date copyright09/11/1992
date issued1992
identifier otherEDYCQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/166661
description abstractDescription of Driving Event:
Failure of relay K41 to activate or relay K44 to deactivate will disable hardwire safing panel control of both the primary and secondary extend pilot valves A101409 and A101410. The command path for the hardwire safing circuits, which controls the orbiter access arm, runs through these relays. If relay K41 fails to activate or relay K44 fails to deactivate, the OAA would not extend. If a failure occurs, the hardwire safing system would not activate the extension circuit and emergency reextension could not be accomplished.
languageEnglish
titleNASA-LLIS-0028num
titleLessons Learned - Extension of Orbiter Access Arm (OAA)en
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1992
contenttypefulltext
subject keywordsFacilities
subject keywordsFlight Equipment
subject keywordsGround Operations
subject keywordsHardware
subject keywordsLaunch Process
subject keywordsLaunch Vehicle


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