1109184

BS HR 209:1989

Specification for nickel-chromium-cobalt-molybdenum-titanium-aluminium heat-resisting alloy sheet, strip and plate: softened (nickel base, Cr 18, Co 14, Mo 7, Ti 2.2, Al 2.1)

standard by BSI Group , 08/31/1989

This document has been replaced. View the most recent version.

View all product details

Historical

Track It

Language:
    • Available Formats
    • Options
    • Availability
    • Priced From ( in USD )
    • Secure PDF 🔒
    • 👥
    • Immediate download
    • $160.02
    • Add to Cart
    • Printed Edition
    • Ships in 1-2 business days
    • $160.02
    • Add to Cart
    • Printed Edition + PDF
    • Immediate download
    • $215.90
    • Add to Cart

Customers Who Bought This Also Bought

 

About This Item

 

Full Description

Chemical composition, mechanical properties and inspection and test requirements for general aerospace use.

Cross References:
BS EN 2500
HR 100
 

Product Details

Published:
08/31/1989
ISBN(s):
058017400X
Number of Pages:
4
File Size:
1 file , 370 KB
Product Code(s):
200393, 200393, 00200393
Note:
This product is unavailable in Ukraine, Russia, Belarus
 

Document History

  1. BS 2HR 209:2011


    Specification for nickel-chromium-cobalt-molybdenum- titanium-aluminium heat-resisting alloy plate, sheet and strip (Nickel base, Cr 18, Co 14, Mo 7, Ti 2.2, Al 2.1)

    • Most Recent

  2. BS HR 209:1989

    👀 currently
    viewing


    Specification for nickel-chromium-cobalt-molybdenum-titanium-aluminium heat-resisting alloy sheet, strip and plate: softened (nickel base, Cr 18, Co 14, Mo 7, Ti 2.2, Al 2.1)

    • Historical Version