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NASA-LLIS-0954
Lessons Learned – Solid Rocket Motor Case-to-Case Field Joint: Added Joint Heate
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:32:57Z | |
| date available | 2017-09-04T18:32:57Z | |
| date copyright | 03/27/1995 | |
| date issued | 1995 | |
| identifier other | JCUEQCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=author:%22NAVY%20-%206159DD6E273C9FCD0Facil/handle/yse/215163 | |
| description abstract | Description of Driving Event: The Challenger (Space Shuttle Flight #51L) accident triggered a detailed review of all of the joints in the Solid Rocket Motor. Analyses showed a potential weakness and potential flow paths for hot gasses through the case-to-nozzle joint that could cause a catastrophic event similar to that encountered in Challenger. | |
| language | English | |
| title | NASA-LLIS-0954 | num |
| title | Lessons Learned – Solid Rocket Motor Case-to-Case Field Joint: Added Joint Heate | en |
| type | standard | |
| page | 2 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1995 | |
| contenttype | fulltext | |
| subject keywords | Energetic Materials - Explosive/Propellant/Pyrotechnic | |
| subject keywords | Launch Vehicle |
