• 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-0773

Lessons Learned – Design Practice to Control Interference from Electrostatic Discharge (ESD)

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

Abstract: Practice:
Minimize the adverse effects of electrostatic discharge (ESD) on spacecraft by implementing the following three design practices:
1. Make all external surfaces of the spacecraft electrically conductive and grounded to the main structure.
2. Provide all internal metallic elements and other conductive elements with an "ESD conductive" path to the main structure.
3. Enclose all sensitive circuitry in an electrically conductive enclosure-- a "Faraday cage".
URI: https://yse.yabesh.ir/std/handle/yse/117749
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (17.30Kb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NASA-LLIS-0773

Show full item record

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:54:17Z
date available2017-09-04T16:54:17Z
date copyright04/11/2000
date issued2000
identifier otherWYCEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/117749
description abstractPractice:
Minimize the adverse effects of electrostatic discharge (ESD) on spacecraft by implementing the following three design practices:
1. Make all external surfaces of the spacecraft electrically conductive and grounded to the main structure.
2. Provide all internal metallic elements and other conductive elements with an "ESD conductive" path to the main structure.
3. Enclose all sensitive circuitry in an electrically conductive enclosure-- a "Faraday cage".
languageEnglish
titleNASA-LLIS-0773num
titleLessons Learned – Design Practice to Control Interference from Electrostatic Discharge (ESD)en
typestandard
page4
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2000
contenttypefulltext
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