Material Control and Fracture Control Planning for the Space Shuttle Orbiter ProgramSource: Journal of Engineering Materials and Technology:;1980:;volume( 102 ):;issue: 001::page 40Author:R. M. Ehret
DOI: 10.1115/1.3224782Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Structural integrity of the Space Shuttle orbiter vehicle is assured primarily through analysis. The analysis is supplemented by tests intended to validate analysis methods or, in some cases, to provide direct demonstration of structural capability to withstand the design environments. The paper summarizes the Shuttle’s structural certification requirements and the major test efforts supporting this certification. A more detailed examination of the orbiter material control land fracture control programs is presented as efficient and constructive components of a viable structural integrity plane.
keyword(s): Fracture (Process) , Vehicles AND Design ,
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| contributor author | R. M. Ehret | |
| date accessioned | 2017-05-08T23:08:54Z | |
| date available | 2017-05-08T23:08:54Z | |
| date copyright | January, 1980 | |
| date issued | 1980 | |
| identifier issn | 0094-4289 | |
| identifier other | JEMTA8-26874#40_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/93394 | |
| description abstract | Structural integrity of the Space Shuttle orbiter vehicle is assured primarily through analysis. The analysis is supplemented by tests intended to validate analysis methods or, in some cases, to provide direct demonstration of structural capability to withstand the design environments. The paper summarizes the Shuttle’s structural certification requirements and the major test efforts supporting this certification. A more detailed examination of the orbiter material control land fracture control programs is presented as efficient and constructive components of a viable structural integrity plane. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Material Control and Fracture Control Planning for the Space Shuttle Orbiter Program | |
| type | Journal Paper | |
| journal volume | 102 | |
| journal issue | 1 | |
| journal title | Journal of Engineering Materials and Technology | |
| identifier doi | 10.1115/1.3224782 | |
| journal fristpage | 40 | |
| journal lastpage | 44 | |
| identifier eissn | 1528-8889 | |
| keywords | Fracture (Process) | |
| keywords | Vehicles AND Design | |
| tree | Journal of Engineering Materials and Technology:;1980:;volume( 102 ):;issue: 001 | |
| contenttype | Fulltext |