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AIAA S-080
Space Systems - Metallic Pressure Vessels, Pressurized Structures, and Pressure Components
Year: 1998
Abstract: Purpose
This standard establishes baseline requirements for the design, fabrication, test, inspection, operation and maintenance of the metallic pressurized hardware used in space systems such as spacecraft and launch vehicles. These requirements when implemented on a particular system, will assure a high level of confidence in achieving safe and reliable operation.
Application
This standard is applicable to space flight metallic pressurized hardware. Included are all pressure vessels, pressurized structures, batteries, heat pipes, cryostats, sealed containers, and pressure components such as lines, fittings, and hoses made of metals. A companion standard, AIAA-S- 081, is applicable to space flight composite overwrapped pressure vessels (COPV).
The requirements specified in this standard may be tailored to specific programs with the agreement of the appropriate approval authority.
This standard establishes baseline requirements for the design, fabrication, test, inspection, operation and maintenance of the metallic pressurized hardware used in space systems such as spacecraft and launch vehicles. These requirements when implemented on a particular system, will assure a high level of confidence in achieving safe and reliable operation.
Application
This standard is applicable to space flight metallic pressurized hardware. Included are all pressure vessels, pressurized structures, batteries, heat pipes, cryostats, sealed containers, and pressure components such as lines, fittings, and hoses made of metals. A companion standard, AIAA-S- 081, is applicable to space flight composite overwrapped pressure vessels (COPV).
The requirements specified in this standard may be tailored to specific programs with the agreement of the appropriate approval authority.
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| contributor author | AIAA - American Institute of Aeronautics and Astronautics | |
| date accessioned | 2017-09-04T15:54:36Z | |
| date available | 2017-09-04T15:54:36Z | |
| date copyright | 1998.01.01 | |
| date issued | 1998 | |
| identifier other | QSWYJAAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jse/handle/yse/57989 | |
| description abstract | Purpose This standard establishes baseline requirements for the design, fabrication, test, inspection, operation and maintenance of the metallic pressurized hardware used in space systems such as spacecraft and launch vehicles. These requirements when implemented on a particular system, will assure a high level of confidence in achieving safe and reliable operation. Application This standard is applicable to space flight metallic pressurized hardware. Included are all pressure vessels, pressurized structures, batteries, heat pipes, cryostats, sealed containers, and pressure components such as lines, fittings, and hoses made of metals. A companion standard, AIAA-S- 081, is applicable to space flight composite overwrapped pressure vessels (COPV). The requirements specified in this standard may be tailored to specific programs with the agreement of the appropriate approval authority. | |
| language | English | |
| title | AIAA S-080 | num |
| title | Space Systems - Metallic Pressure Vessels, Pressurized Structures, and Pressure Components | en |
| type | standard | |
| page | 28 | |
| status | Active | |
| tree | AIAA - American Institute of Aeronautics and Astronautics:;1998 | |
| contenttype | fulltext |