درباره ما
NASA-LLIS-0180
Lessons Learned - Solid Rocket Motor (SRM) Sealing Surfaces
Year: 1992
Abstract: Description of Driving Event:
A case dimensional change study performed as part of the 51-L failure analysis effort produced the diameter change results. The potential cause for this phenomenon is believed to be material related in three areas and their direct effect on the hydrostatic proof test pressure level chosen for acceptance testing prior to reuse.
A case dimensional change study performed as part of the 51-L failure analysis effort produced the diameter change results. The potential cause for this phenomenon is believed to be material related in three areas and their direct effect on the hydrostatic proof test pressure level chosen for acceptance testing prior to reuse.
Subject: Hardware
Show full item record
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:49:45Z | |
| date available | 2017-09-04T15:49:45Z | |
| date copyright | 33900 | |
| date issued | 1992 | |
| identifier other | QEZCQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/52782 | |
| description abstract | Description of Driving Event: A case dimensional change study performed as part of the 51-L failure analysis effort produced the diameter change results. The potential cause for this phenomenon is believed to be material related in three areas and their direct effect on the hydrostatic proof test pressure level chosen for acceptance testing prior to reuse. | |
| language | English | |
| title | NASA-LLIS-0180 | num |
| title | Lessons Learned - Solid Rocket Motor (SRM) Sealing Surfaces | en |
| type | standard | |
| page | 2 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1992 | |
| contenttype | fulltext | |
| subject keywords | Hardware | |
| subject keywords | Parts Materials & Processes |