SAE AMS4899
Titanium Alloy, Sheet, Strip, and Plate 4.5al 3v 2fe 2mo Annealed.
Standard:
AKA:
- AMS4899
- 1996-04-01
- Historical. Access the latest revision: AMS4899C
- Ams G Titanium And Refractory Metals Committee
This specification covers a titanium alloy in the form of sheet, strip, and plate.
These products have been used typically for parts requiring high fracture toughness, fatigue strength, formability, and strenth up to 480 degrees F (249 degrees C), but usage is not limited to such applications. The alloy is superplastic below 1520 degrees F (827 degrees C) and hot formable from 1200 to 1560 degrees F (649 to 849 degrees C).
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4899C | 2011-09-13 | Latest | |
| AMS4899B | 2007-10-16 | Historical | |
| AMS4899A | 2003-01-07 | Historical | |
| AMS4899 | 1996-04-01 | Historical |
- SAE AMS 4899
- Aerospace
- Nonferrous alloys
- Titanium alloys