BS 2S 98:1964 PDF

Name:
BS 2S 98:1964 PDF

Published Date:
01/31/1964

Status:
Active

Description:

Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)

Publisher:
BSI Group

Document status:

Active

Format:

Electronic (PDF)

Delivery time:

10 minutes

Delivery time (for Russian version):

200 business days

SKU:

Cross References:
BS 350
3S 100

Replaces BS S 98:1949.

File Size :	1 file , 260 KB
ISBN(s) :	0580344657
Note :	This product is unavailable in Ukraine, Russia, Belarus
Number of Pages :	6
Product Code(s) :	124150, 124150, 00124150
Published :	01/31/1964

Published Date: 01/31/1964

Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)

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1 % Chromium-molybdenum steel billets, bars, forgings and parts. (1150 to 1300 MPa: Limiting ruling section 16 mm) (Suitable for welding)

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Aerospace series. Steel FE-PM3801 (X5CrNiCu17-4). Air melted, solution treated and precipitation treated, bar a or D ≤ 200 mm, Rm ≥ 1310 MPa

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