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WL 1.6657-100
Aerospace; case-hardening nickel-chromium-molydenum steel with approx. 0,14 C, 3 Ni, 1 Cr, 0,2 Mo; bars and forgings; design and production data, conversion
Edition
1992-08
WL 1.6658-1
Aerospace; case-hardening nickel-chromium-molydenum steel with approx. 0,14 C, 3 Ni, 1 Cr, 0,2 Mo, consumable electrode remelted; bars and forgings
Edition
1992-08
WL 1.6658-100
Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,14 C, 3 Ni, 1 Cr, 0,2 Mo, consumable electrode remelted; bars and forgings; design and production data, conversion
Edition
1992-08
WL 1.6722-1
Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,15 C, 4 Ni, 1 Cr, 0,2 Mo, comsumable electrode remelted; bars and forgings
Edition
1992-08
WL 1.6722-100
Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,15 C, 4 Ni, 1 Cr, 0,2 Mo, comsumable electrode remelted; bars and forgings; design and production data, conversion
Edition
1992-08
WL 1.6723-1
Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,15 C, 4 Ni, 1 Cr, 0,2 Mo; bars and forgings
Edition
1992-08
WL 1.6723-100
Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,15 C, 4 Ni, 1 Cr, 0,2 Mo; bars and forgings; design and production data, conversion
Edition
1992-08
WL 1.6944 Beiblatt 1
Ultra high-strength nickel-chromium-molybdenum steel with about 0.38C-1.8Ni-0.8Cr-0.35Mo-0,1V; sheets, plates, rods, forgings, pipes, filler metal
Edition
1984-07
WL 1.6944-1
Ultra high-strength nickel-chromium-molybdenum steel with about 0.38C-1.8Ni-0.8Cr-0.35Mo-0.1V; sheets and plates
Edition
1984-07
WL 1.6944-2
Ultra high-strength nickel-chromium-molybdenum steel with about 0.38C-1.8Ni-0.8Cr-0.35Mo-0.1V; rods and forgings
Edition
1984-07
