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Lessons Learned – Failure of Pyrotechnic Operated Valves with Dual Initiators

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:32:17Z
date available2017-09-04T16:32:17Z
date copyright05/11/2009
date issued2009
identifier otherUQYCQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/95687
description abstractAbstract:
Four spacecraft propulsion system pyrovalve no-fire failures were investigated by the NESC (NASA Engineering and Safety Center). In all four cases, a normally closed pyrovalve failed to actuate during tests in which simultaneous firing of dual initiators failed to ignite the booster charge. Timing of redundant initiator firings is crucial for reliable operation of pyrovalves. Dual simultaneous firing (less than 10 microseconds skew) is not as robust as a single firing and should be avoided.
languageEnglish
titleNASA-LLIS-2045num
titleLessons Learned – Failure of Pyrotechnic Operated Valves with Dual Initiatorsen
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2009
contenttypefulltext
subject keywordsAdditional Categories.Energetic Materials - Explosive/Propellant/Pyrotechnic
subject keywordsAdditional Categories.Hardware
subject keywordsAdditional Categories.Spacecraft


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