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Thrust chamber life prediction. volume 1: mechanical and physical properties of high performance rocket nozzle materials
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Zabora, R. F. Esposito, J. J. |
| Copyright Year | 1975 |
| Description | Pertinent mechanical and physical properties of six high conductivity metals were determined. The metals included Amzirc, NARloy Z, oxygen free pure copper, electroformed copper, fine silver, and electroformed nickel. Selection of these materials was based on their possible use in high performance reusable rocket nozzles. The typical room temperature properties determined for each material included tensile ultimate strength, tensile yield strength, elongation, reduction of area, modulus of elasticity, Poisson's ratio, density, specific heat, thermal conductivity, and coefficient of thermal expansion. Typical static tensile stress-strain curves, cyclic stress-strain curves, and low-cycle fatigue life curves are shown. Properties versus temperature are presented in graphical form for temperatures from 27.6K (-410 F) to 810.9K (1000 F). |
| File Size | 1122526 |
| Page Count | 54 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750021165 |
| Archival Resource Key | ark:/13960/t0zp8t245 |
| Language | English |
| Publisher Date | 1975-03-01 |
| Access Restriction | Open |
| Subject Keyword | Metallic Materials Fatigue Tests Rocket Nozzles Silver Nickel Alloys Life Durability Performance Prediction Mechanical Properties Thrust Chambers Copper Thermophysical Properties 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 |
