• 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-0592

Lessons Learned – Conformal Coating as Moisture Protection of Electronic Circuitry in Micro Gravity

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1998

Abstract: Description of Driving Event:
The Microgravity Smoldering Combustion protoflight unit was flown on the STS69 shuttle mission. Resulting flight data indicated anomalous readings from two thermocouples. Both channels had noticeable noise, and readings, which were higher than anticipated for the condition. Since the igniter algorithm uses this information to initiate igniter shut-off the igniter was shut off prior to establishing desired conditions in the foam for smoldering completion.
URI: https://yse.yabesh.ir/std/handle/yse/119954
Subject: Parts Materials & Processes
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (13.49Kb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NASA-LLIS-0592

Show full item record

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:56:30Z
date available2017-09-04T16:56:30Z
date copyright06/17/1998
date issued1998
identifier otherXECEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/119954
description abstractDescription of Driving Event:
The Microgravity Smoldering Combustion protoflight unit was flown on the STS69 shuttle mission. Resulting flight data indicated anomalous readings from two thermocouples. Both channels had noticeable noise, and readings, which were higher than anticipated for the condition. Since the igniter algorithm uses this information to initiate igniter shut-off the igniter was shut off prior to establishing desired conditions in the foam for smoldering completion.
languageEnglish
titleNASA-LLIS-0592num
titleLessons Learned – Conformal Coating as Moisture Protection of Electronic Circuitry in Micro Gravityen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1998
contenttypefulltext
subject keywordsParts Materials & Processes
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