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Lessons Learned - Galileo Spacecraft Telemetry Degradation due to Antenna Multipath

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:49:05Z
date available2017-09-04T17:49:05Z
date copyright34649
date issued1994
identifier otherETAEQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/172303
description abstractAbstract:
After Galileo completed its second Earth flyby, communication signal levels received on Earth decreased and fluctuated unexpectedly. The cause was determined to be interference that was not detected during test because the test article was not consistent with the orbiter telecommunications functional requirements document.
Recommendations involved use of concurrent engineering, verification of requirements compliance, updating of requirements documents based on hardware ECR's, post test evaluation of non-flight like characteristics, and assuring that hardware used for functional testing properly simulates the characteristics of the flight hardware.
languageEnglish
titleNASA-LLIS-0350num
titleLessons Learned - Galileo Spacecraft Telemetry Degradation due to Antenna Multipathen
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1994
contenttypefulltext
subject keywordsCommunication Systems
subject keywordsConfiguration Management
subject keywordsRF Performance Verification
subject keywordsTest & Verification


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