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NASA-LLIS-0705

Lessons Learned – Micrometeoroid Protection

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 2000

Abstract: Abstract:
Preferred Practice for Design & Test. The absence of micrometeoroid protection measures in spacecraft and mission design will increase the risk of significant damage to the spacecraft, particularly in areas of high meteoroid flux and during vulnerable mission phases.
Provide protection for the spacecraft structure and instruments to minimize damage from micrometeoroid penetration. Typical reliability engineering measures range from structural positioning to protect sensitive hardware to placement of protective blankets on the spacecraft exterior.
URI: https://yse.yabesh.ir/std/handle/yse/124467
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    NASA-LLIS-0705

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:00:58Z
date available2017-09-04T17:00:58Z
date copyright03/16/2000
date issued2000
identifier otherXQCEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/124467
description abstractAbstract:
Preferred Practice for Design & Test. The absence of micrometeoroid protection measures in spacecraft and mission design will increase the risk of significant damage to the spacecraft, particularly in areas of high meteoroid flux and during vulnerable mission phases.
Provide protection for the spacecraft structure and instruments to minimize damage from micrometeoroid penetration. Typical reliability engineering measures range from structural positioning to protect sensitive hardware to placement of protective blankets on the spacecraft exterior.
languageEnglish
titleNASA-LLIS-0705num
titleLessons Learned – Micrometeoroid Protectionen
typestandard
page9
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2000
contenttypefulltext
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DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
yabeshDSpacePersian