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High toughness-high strength iron alloy
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Stephens, J. R. |
| Copyright Year | 1980 |
| Description | An iron alloy is provided which exhibits strength and toughness characteristics at cryogenic temperatures. The alloy consists essentially of about 10 to 16 percent by weight nickel, about 0.1 to 1.0 percent by weight aluminum, and 0 to about 3 percent by weight copper, with the balance being essentially iron. The iron alloy is produced by a process which includes cold rolling at room temperature and subsequent heat treatment. |
| File Size | 344389 |
| Page Count | 4 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800023976 |
| Archival Resource Key | ark:/13960/t6838mg73 |
| Language | English |
| Publisher Date | 1980-07-29 |
| Access Restriction | Open |
| Subject Keyword | Metallic Materials Low Temperature Tests Cold Rolling Heat Treatment Nickel Alloys Cryogenics Yield Strength Iron Alloys Fracture Strength High Strength Alloys Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |
