BS S 128:1964 - Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)

BS S 128:1964

Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)

Status : Withdrawn   Published : January 1964

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Standard NumberBS S 128:1964
TitleSpecification for aircraft material. 24/17 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
StatusWithdrawn
Publication Date31 January 1964
Withdrawn Date15 March 1999
Normative References(Required to achieve compliance to this standard)No other standards are normatively referenced
Informative References(Provided for Information)No other standards are informatively referenced
Amended ByPD 6333
Draft Superseded ByD62/3645 DC
DescriptorsSteels, Alloy steels, Chromium steels, Nickel steels, Niobium-containing alloys, Heat-resistant materials, Stainless steels, Tensile strength, Bars (materials), Billets, Forgings, Aircraft components, Air transport engineering, Chemical composition, Designations, Mechanical properties of materials, Artificial ageing tests
ICS49.025.10
Title in FrenchMateriau pour aeronefs. Specification. Acier resistant a la chaleur a 24/17 chrome-nickel (stabilise au niobium) (35 tonf/sq in: section limite 6 pouces)
Title in GermanFlugzeugmaterial. Spezifikation. Hitzefester 24/17 Chrom-Nickelstahl (niob-stabilisiert) (35 tonf/sq in; hoechstzulaessiges Profil 6 Zoll)
CommitteeACE/61/-/15
PublisherBSI
FormatA4
DeliveryNo
Pages5
File Size336.5 KB
Price£110.00


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