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NASA-LLIS-0613
Lessons Learned – Solid Rocket Booster, Bonding Material Process
Year: 1997
Abstract: Description of Driving Event:
To meet environmental requirements, a program decision was made to change the Pressure Sensitive Adhesive used in the J-flap of the segment of the Shuttle Reusable Solid Rocket Motor (RSRM) and the solvent used in the joint cleaning process. A new Pressure Sensitive Adhesive was acquired and a solvent-based cleaning wipe was replaced with an aqueous-based joint cleaning process. Post flight analysis of the RSRM flight article revealed greater than expected erosion, sooting and heat effects on the insulation interfaces.
To meet environmental requirements, a program decision was made to change the Pressure Sensitive Adhesive used in the J-flap of the segment of the Shuttle Reusable Solid Rocket Motor (RSRM) and the solvent used in the joint cleaning process. A new Pressure Sensitive Adhesive was acquired and a solvent-based cleaning wipe was replaced with an aqueous-based joint cleaning process. Post flight analysis of the RSRM flight article revealed greater than expected erosion, sooting and heat effects on the insulation interfaces.
Subject: Environment
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:52:08Z | |
| date available | 2017-09-04T15:52:08Z | |
| date copyright | 04/20/1997 | |
| date issued | 1997 | |
| identifier other | QMCEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/55432 | |
| description abstract | Description of Driving Event: To meet environmental requirements, a program decision was made to change the Pressure Sensitive Adhesive used in the J-flap of the segment of the Shuttle Reusable Solid Rocket Motor (RSRM) and the solvent used in the joint cleaning process. A new Pressure Sensitive Adhesive was acquired and a solvent-based cleaning wipe was replaced with an aqueous-based joint cleaning process. Post flight analysis of the RSRM flight article revealed greater than expected erosion, sooting and heat effects on the insulation interfaces. | |
| language | English | |
| title | NASA-LLIS-0613 | num |
| title | Lessons Learned – Solid Rocket Booster, Bonding Material Process | en |
| type | standard | |
| page | 2 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1997 | |
| contenttype | fulltext | |
| subject keywords | Environment | |
| subject keywords | Parts Materials & Processes |