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High-pressure oxygen test evaluations. [impact tests/metals - space shuttles
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Schwinghamer, R. J. Key, C. F. |
| Copyright Year | 1974 |
| Description | The relevance of impact sensitivity testing to the development of the space shuttle main engine is discussed in the light of the special requirements for the engine. The background and history of the evolution of liquid and gaseous oxygen testing techniques and philosophy is discussed also. The parameters critical to reliable testing are treated in considerable detail, and test apparatus and procedures are described and discussed. Materials threshold sensitivity determination procedures are considered and a decision logic diagram for sensitivity threshold determination was plotted. Finally, high-pressure materials sensitivity test data are given for selected metallic and nonmetallic materials. |
| File Size | 3181099 |
| Page Count | 27 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750023136 |
| Archival Resource Key | ark:/13960/t9j43j513 |
| Language | English |
| Publisher Date | 1974-11-29 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Oxygen Sensitivity Lubricants Drop Tests Metals Space Shuttles Impact Tests Impact Testing Machines Cryogenic Rocket Propellants High Pressure 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 |
