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NASA-LLIS-0701
Lessons Learned - Static Cryogenic Seals for Launch Vehicle Applications
Year: 2000
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.
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.
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| 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 |