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NASA-LLIS-0701
Lessons Learned - Static Cryogenic Seals for Launch Vehicle Applications
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:02:13Z | |
| date available | 2017-09-04T16:02:13Z | |
| date copyright | 03/15/2000 | |
| date issued | 2000 | |
| identifier other | RNCEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/65415 | |
| description abstract | Practice: Deflection actuated, pressure assisted coated metal seals, or spring energized Teflon® seals, along with prudent flange joint designs, should be used for high pressure static cryogenic sealing applications in launch vehicle engines and related propulsion system components. | |
| language | English | |
| title | NASA-LLIS-0701 | num |
| title | Lessons Learned - Static Cryogenic Seals for Launch Vehicle Applications | en |
| type | standard | |
| page | 13 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |
