• 0
    • ارسال درخواست
    • حذف همه
    • Industrial Standards
    • Defence Standards
  • درباره ما
  • درخواست موردی
  • فهرست استانداردها
    • Industrial Standards
    • Defence Standards
  • راهنما
  • Login
  • لیست خرید شما 0
    • ارسال درخواست
    • حذف همه
View Item 
  •   YSE
  • Defence Standards
  • NASA - National Aeronautics and Space Administration (NASA)
  • View Item
  •   YSE
  • Defence Standards
  • NASA - National Aeronautics and Space Administration (NASA)
  • View Item
  • All Fields
  • Title(or Doc Num)
  • Organization
  • Year
  • Subject
Advanced Search
JavaScript is disabled for your browser. Some features of this site may not work without it.

Archive

NASA-LLIS-0546

Lessons Learned – Venting Design for Small Pressure Changes

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1996

Abstract: Description of Driving Event:
The MIDAS experiment was designed for one atmosphere pressure, and thus venting was not seen as a requirement and was not designed in. However, the specified minimum and maximum pressures on Shuttle and Mir would have produced a potential maximum pressure difference of 4 psi in the worst case. Venting was back-designed into the system after the fact, when this was determined.
URI: http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/203242
Subject: Environment
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (12.77Kb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NASA-LLIS-0546

Show full item record

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:20:40Z
date available2017-09-04T18:20:40Z
date copyright04/01/1996
date issued1996
identifier otherHXBEQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/203242
description abstractDescription of Driving Event:
The MIDAS experiment was designed for one atmosphere pressure, and thus venting was not seen as a requirement and was not designed in. However, the specified minimum and maximum pressures on Shuttle and Mir would have produced a potential maximum pressure difference of 4 psi in the worst case. Venting was back-designed into the system after the fact, when this was determined.
languageEnglish
titleNASA-LLIS-0546num
titleLessons Learned – Venting Design for Small Pressure Changesen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1996
contenttypefulltext
subject keywordsEnvironment
subject keywordsFlight Equipment
subject keywordsHardware
DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
yabeshDSpacePersian
 
DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
yabeshDSpacePersian