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Lessons Learned – Probable Scenario for Mars Polar Lander Mission Loss (1998)

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:22:00Z
date available2017-09-04T15:22:00Z
date copyright02/15/2001
date issued2001
identifier otherNAUEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/22018
description abstractAbstract:
Neither the MPL software requirements specification nor the software, subsystem or system test plans required verification of immunity to transient signals. MPL touchdown sensors generated known transient signals at leg deployment. Full leg deployment test was not repeated after wiring corrections. Tests should be re-run after test deficiencies are corrected or hardware or software is revised unless clear rationale exists for not doing so. Hardware operational characteristics, including transients and spurious signals must be reflected in software requirements and verified by test.
languageEnglish
titleNASA-LLIS-0938num
titleLessons Learned – Probable Scenario for Mars Polar Lander Mission Loss (1998)en
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2001
contenttypefulltext
subject keywordsFlight Equipment
subject keywordsHardware
subject keywordsPolicy & Planning
subject keywordsRisk Management/Assessment
subject keywordsSafety & Mission Assurance
subject keywordsSoftware
subject keywordsSoftware Test
subject keywordsSpacecraft
subject keywordsSystem Integration and Test
subject keywordsTest & Verification
subject keywordsTest Article
subject keywordsTest Planning


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