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Normas BSI – AENOR
BS 2S 119:1964

BS 2S 119:1964

Specification for aircraft material. 1$9H per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 2$9H in)

Fecha Anulación:
1999-03-15 /Withdrawn
Comité:
ACE/61/-/15
Keywords:
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
71,87
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