Steel bars, 0.95Cr 0.20Mo (0.38-0.43c) normalized. (SAE standard)
Technical Report
·
OSTI ID:591037
This specification covers an aircraft-quality, low-alloy steel in the form of bars. These bars have been used typically for parts 0.50 inch (12.7 mm) and under in section thickness at time of heat treatment requiring a through-hardening steel capable of developing hardness as high as 50 HRC when properly hardened and tempered and also for parts of greater thickness requiring proportionately lower hardness, but usage is not limited to such applications. Alloy: 4140 UNS Number: G4140.
- Research Organization:
- Society of Automotive Engineers, Inc., Warrendale, PA (United States)
- OSTI ID:
- 591037
- Report Number(s):
- SAE-AMS-6349B/XAB; TRN: 80903334
- Resource Relation:
- Other Information: DN: Copyright Society for Automotive Engineers (SAE), 400 Commonwealth Drive, Warrendale, PA. 15096, USA. This document is available from NTIS under license from SAE. See also MIL-S-5626; PBD: Oct 1993
- Country of Publication:
- United States
- Language:
- English
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OSTI ID:591037