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Validation testing of shallow notched round-bar screening test specimens. [for the space shuttle main engine
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Vroman, G. A. |
| Copyright Year | 1975 |
| Description | The capability of shallow-notched, round-bar, tensile specimens for screening critical environments as they affect the material fracture properties of the space shuttle main engine was tested and analyzed. Specimens containing a 0.050-inch-deep circumferential sharp notch were cyclically loaded in a 5000-psi hydrogen environment at temperatures of +70 and -15 F. Replication of test results and a marked change in cyclic life because of temperature variation demonstrated the validity of the specimen type to be utilized for screening tests. |
| File Size | 5646818 |
| Page Count | 27 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750019355 |
| Archival Resource Key | ark:/13960/t08w8661x |
| Language | English |
| Publisher Date | 1975-06-06 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Critical Pressure Metal Plates Space Shuttles Life Durability Tensile Tests Environment Effects Notch Tests Fracture Strength Crack Propagation Bars Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |