BS 2S 98:1964
$86.31
Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)
Published By | Publication Date | Number of Pages |
BSI | 1964 | 8 |
Status | Withdrawn |
---|---|
Pages | 8 |
Publication Date | 1964-01-31 |
Withdrawn Date | 2014-12-31 |
Replaced By | BS 3S 98:2014 |
ISBN | 0 580 34465 7 |
Standard Number | BS 2S 98:1964 |
Title | Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in) |
Descriptors | Heat treatment, Designations, Chromium steels, Mechanical properties of materials, Forgings, Chemical composition, High-carbon steels, Aircraft components, Nickel steels, Molybdenum steels, Steels, Billets, Tensile strength, Hardness, Bars (materials) |
Publisher | BSI |
Committee | ACE/61/-/15 |
ICS Codes | 49.025.10 - Steels |