BS 2S 120:1964

Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (oil hardening) (100 tonf/sq in: limiting ruling section 2½ in)

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Product Details

Descriptors

Billets

Alloy steels

Nickel steels

Bars (materials)

Air transport engineering

Low-alloy steels

Aircraft components

Steels

Molybdenum steels

Heat treatment

Hardness

Forgings

Hardening

Chemical composition

Tensile strength

Chromium steels

Designations

Mechanical properties of materials

ICS Codes

49.025.10 Steels

Committee

ACE/61/-/15

International relationships

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ISBN

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Publisher

BSI