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Lessons Learned - Voyager Subsystem Interface Noise Problems

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:34:37Z
date available2017-09-04T18:34:37Z
date copyright03/21/1995
date issued1995
identifier otherJHBEQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho1/handle/yse/216799
description abstractAbstract:
Problems due to waveform irregularities and the resultant induced noise on the Voyager Spacecraft system interfaces were not validated until 500 hours of system testing had been completed. Lessons involve the need for early system tests to determine subsystem compatibility and design requirements for electrical noise and transients, and extensive interface testing under flight-like conditions.
languageEnglish
titleNASA-LLIS-0390num
titleLessons Learned - Voyager Subsystem Interface Noise Problemsen
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1995
contenttypefulltext
subject keywordsSpacecraft
subject keywordsTest & Verification


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