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NASA-LLIS-1402

Lessons Learned - NASA Engineering and Safety Center Consultation on Mars Exploration Rover Entry, Descent and Landing

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 2004

Abstract: Abstract:
Engineering sensors included on board the Spirit and Opportunity Mars Exploration Rovers were inadequate to allow an unambiguous physical reconstruction of vehicle performance during the critical entry, descent and landing phase. Suitable sensors to measure pressure, temperature and/or other key variables of the local environment, should be included on future landed missions.
URI: https://yse.yabesh.ir/std/handle/yse/22786
Subject: Flight Operations
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  • NASA - National Aeronautics and Space Administration (NASA)
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    NASA-LLIS-1402

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:22:37Z
date available2017-09-04T15:22:37Z
date copyright05/10/2004
date issued2004
identifier otherNCWEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/22786
description abstractAbstract:
Engineering sensors included on board the Spirit and Opportunity Mars Exploration Rovers were inadequate to allow an unambiguous physical reconstruction of vehicle performance during the critical entry, descent and landing phase. Suitable sensors to measure pressure, temperature and/or other key variables of the local environment, should be included on future landed missions.
languageEnglish
titleNASA-LLIS-1402num
titleLessons Learned - NASA Engineering and Safety Center Consultation on Mars Exploration Rover Entry, Descent and Landingen
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2004
contenttypefulltext
subject keywordsFlight Operations
subject keywordsHardware
subject keywordsProgram and Project Management
subject keywordsRisk Management/Assessment
subject keywordsSafety & Mission Assurance
subject keywordsSpacecraft
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DSpace software copyright © 2017-2020  DuraSpace
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