BS 2S 119:1964

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Specification for aircraft material. 1½ per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 2½ in)

Published By	Publication Date	Number of Pages
BSI	1964	3

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Categories: 49.025.10 - Steels, BSI

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Additional information

Status	Withdrawn
Pages	3
Publication Date	1964-01-31
Withdrawn Date	1999-03-15
Standard Number	BS 2S 119:1964
Title	Specification for aircraft material. 1½ per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 2½ in)
Descriptors	Mechanical properties of materials, Heat treatment, Designations, Steels, Chemical composition, Molybdenum steels, Bars (materials), Aircraft components, Air transport engineering, Hardness, Tensile strength, Nickel steels, Low-alloy steels, Chromium steels, Billets, Forgings, Alloy steels
Publisher	BSI
Committee	ACE/61/-/15
ICS Codes	49.025.10 - Steels

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BS 2S 119:1964

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