Specification for chromium-nickel-molybdenum-vanadium heat-resisting steel sheet and strip (930-1130 MPa: maximum thickness 6 mm) (Cr 12, Ni 2.5, Mo 1.7, V 0.3)

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English

Published date

09-12-2003

Publisher

British Standards Institution

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Describes manufacture, inspection and testing of heat resisting alloys for aerospace purposes. Gives chemical composition and mechanical properties. This covers chromium nickel molybdenum vanadium sheet and strip.

Committee	ACE/61/-/15
DevelopmentNote	Supersedes 02/711475 DC, 73/32574 DC and DTD 5046. (12/2003) Reviewed and confirmed by BSI, December 2012. (11/2012)
DocumentType	Standard
Pages	8
PublisherName	British Standards Institution
Status	Current
Supersedes	DTD 5046 : LATEST 02/711475 DC : DRAFT OCT 2002

BS 4S 500:2010

Aerospace series. Procedure for inspection, testing and acceptance of steel sheet and strip

BS S500(1956) : LATEST

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BS S 538:1975

Specification for chromium-nickel-molybdenum-vanadium heat-resisting steel sheet and strip (930-1130 MPa: maximum thickness 6 mm) (Cr 12, Ni 2.5, Mo 1.7, V 0.3)

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BS S 538:1975

Specification for chromium-nickel-molybdenum-vanadium heat-resisting steel sheet and strip (930-1130 MPa: maximum thickness 6 mm) (Cr 12, Ni 2.5, Mo 1.7, V 0.3)

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