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Lessons Learned - Back Pressure Regulato

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:15:44Z
date available2017-09-04T17:15:44Z
date copyright09/18/1992
date issued1992
identifier otherZDYCQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/139152
description abstractDescription of Driving Event:
The T-0 vent support assemblies are mounted on the orbiter T-0 Interface to support controlled venting of PRSD tanks after landing. In the event of regulator diaphragm failure, GH2 or GO2 can vent to atmosphere near the orbiter through the back pressure regulators. Leaking GH2 could cause a fire or explosion. Leaking GO2 could contribute to failure of the diaphragm in the back pressure regulator of the FCSS, PRSD T-0 safing system could release GH2 in the vicinity of the orbiter.
languageEnglish
titleNASA-LLIS-0036num
titleLessons Learned - Back Pressure Regulatoen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1992
contenttypefulltext
subject keywordsEnergetic Materials - Explosive/Propellant/Pyrotechnic
subject keywordsFacilities
subject keywordsFlight Equipment
subject keywordsGround Equipment
subject keywordsGround Operations
subject keywordsHardware
subject keywordsHazardous/Toxic Waste/Materials
subject keywordsLaunch Vehicle
subject keywordsParts Materials & Processes
subject keywordsPressure Vessel


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