BS 2S 119:1964

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

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Product Details

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

ICS Codes

49.025.10 Steels

Committee

ACE/61/-/15

International relationships

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ISBN

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Publisher

BSI