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Lessons Learned - External filter needed to achieve low EMI from TWTA

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:39:00Z
date available2017-09-04T18:39:00Z
date copyright09/26/2008
date issued2008
identifier otherJQXCQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho162sAF679D40AC421854DD6EFDEC9FCD/handle/yse/220647
description abstractAbstract:
The Lunar Reconnaissance Orbiter required lower levels of Electromagnetic Interference (EMI) than usual to avoid causing sensitive components to malfunction. It was found necessary to use an external filter between the bus and the EPC of the TWTA to obtain the needed level of EMI.
languageEnglish
titleNASA-LLIS-1864num
titleLessons Learned - External filter needed to achieve low EMI from TWTAen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2008
contenttypefulltext
subject keywordsEngineering Design (Phase C/D).Spacecraft and Spacecraft Instruments
subject keywordsIntegration and Testing


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