Show simple item record

Ceramic Column Grid Array Design and Manufacturing Rules for Flight Hardware

contributor authorGSFC - NASA - GSFC - Robert H. Goddard Space Flight Center
date accessioned2017-09-04T16:08:48Z
date available2017-09-04T16:08:48Z
date copyright02/22/2011
date issued2011
identifier otherSFDNUEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/72073
description abstractPurpose
The purpose of this standard is to provide requirements and recommendations intended to facilitate production of defect-free ceramic column grid array solder joint interconnects to boards intended for use in space flight applications (refer to Appendix A, Technology Background). This standard does not provide application specific reliability test requirements (e.g. qualification requirements).
Applicability
This standard is applicable to all uses on flight hardware of ceramic packaged electronic parts which are solder-attached to printed circuit boards with solder columns (ceramic column grid array attachments or CCGAs).
languageEnglish
titleGSFC-STD-6001num
titleCeramic Column Grid Array Design and Manufacturing Rules for Flight Hardwareen
typestandard
page21
statusActive
treeGSFC - NASA - GSFC - Robert H. Goddard Space Flight Center:;2011
contenttypefulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record