• 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-0390

Lessons Learned - Voyager Subsystem Interface Noise Problems

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1995

Abstract: Abstract:
Problems due to waveform irregularities and the resultant induced noise on the Voyager Spacecraft system interfaces were not validated until 500 hours of system testing had been completed. Lessons involve the need for early system tests to determine subsystem compatibility and design requirements for electrical noise and transients, and extensive interface testing under flight-like conditions.
URI: http://yse.yabesh.ir/std;query=autho1/handle/yse/216799
Subject: Spacecraft
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (14.96Kb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NASA-LLIS-0390

Show full item record

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:34:37Z
date available2017-09-04T18:34:37Z
date copyright03/21/1995
date issued1995
identifier otherJHBEQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho1/handle/yse/216799
description abstractAbstract:
Problems due to waveform irregularities and the resultant induced noise on the Voyager Spacecraft system interfaces were not validated until 500 hours of system testing had been completed. Lessons involve the need for early system tests to determine subsystem compatibility and design requirements for electrical noise and transients, and extensive interface testing under flight-like conditions.
languageEnglish
titleNASA-LLIS-0390num
titleLessons Learned - Voyager Subsystem Interface Noise Problemsen
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1995
contenttypefulltext
subject keywordsSpacecraft
subject keywordsTest & Verification
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