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Lessons Learned - Orbiter Compartment Overpressurization

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:24:46Z
date available2017-09-04T16:24:46Z
date copyright08/21/1992
date issued1992
identifier otherTVYCQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/88024
description abstractDescription of Driving Event:
The portable purge unit supplies conditioned air through ducts to the orbiter to purge and/or pressurize the payload bay's forward and aft compartments. Airflow varies between 50 lbs/min minimum to 100 lbs/min maximum. Vent door observers are always on station when a vent door is repositioned for a test or TPS tile/thermal barrier work. Overpressurization may occur if all the orbiter vent doors (normally in the purge position) for a compartment are closed at one time. Control logic program VAM09 also notifies the firing room engineers if both a right hand and left hand purge vent door set is closed.
languageEnglish
titleNASA-LLIS-0125num
titleLessons Learned - Orbiter Compartment Overpressurizationen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1992
contenttypefulltext
subject keywordsGround Operations
subject keywordsLaunch Vehicle


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