Show simple item record

Lessons Learned - Debonding Due to Pressure Trapped in Voids with Subsequent Exposure to External Reduced Pressure

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:18:04Z
date available2017-09-04T15:18:04Z
date copyright06/14/1993
date issued1993
identifier otherMPAEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/17620
description abstractDescription of Driving Event:
KSC post flight inspections of RSRM-2 (STS 27) showed a 3.5" x 3.5" piece of JPS cork missing from the right hand center field joint at 185 degrees indicating debris. An unbond also existed between the EPDM moisture seal and the extruded cork at this missing location. The missing cork was located at the kevlar band buckle, where the JPS cork interface had been cut to fit over the buckle, creating an unvented void area under the cork.
languageEnglish
titleNASA-LLIS-0330num
titleLessons Learned - Debonding Due to Pressure Trapped in Voids with Subsequent Exposure to External Reduced Pressureen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1993
contenttypefulltext
subject keywordsHardware
subject keywordsParts Materials & Processes


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record