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Lessons Learned - Procedure Devolvement over Time in a Seriesed Spacecraft Program

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:11:00Z
date available2017-09-04T17:11:00Z
date copyright02/03/2012
date issued2012
identifier otherYROMUEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/134615
description abstractNational Oceanic and Atmospheric Administration (NOAA) N-Prime is one of a series of satellites built by the Goddard Space Flight Center (GSFC) and uses handling procedures originally developed at the program‟s outset. The spacecraft has a deploy-able Search and Rescue Antenna (SRA) which was originally "hard stowed" using a non-flight bolt and Tnut in the baselined procedure. The procedure was progressively modified and devolved over time due to the changing GSE availability and allowed for using a lance cord in lieu of the hard stow to secure the antenna in a "soft stow". During ground operations the spacecraft was rotated and the SRA inadvertently deployed when the cord broke. The SRA broke through a hard stop bracket and damaged an instrument optical sensor radiator panel. The satellite damage was minimal and there were no injuries to personnel. A Mishap Investigation Board (MIB) was commissioned to investigate this mishap. Their findings form the basis for this lesson.
languageEnglish
titleNASA-LLIS-6256num
titleLessons Learned - Procedure Devolvement over Time in a Seriesed Spacecraft Programen
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2012
contenttypefulltext
subject keywordsIntegration and Testing
subject keywordsMission Operations and Ground Support Systems.Crew Operations
subject keywordsMission Operations and Ground Support Systems.Ground processing and manifesting
subject keywordsMission Operations and Ground Support Systems.Ground support systems


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