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

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

Aerospace; high-strength hardened and tempered nickel-cobalt steel with approx. 0,3 C, 8 Ni, 4,5 Co, 1 Cr, 1 Mo, consumable electrode remelted; bars and forgings
Edition 1992-08

Aerospace; high-strength hardened and tempered nickel-cobalt steel with approx. 0,3 C, 8 Ni, 4,5 Co, 1 Cr, 1 Mo, consumable electrode remelted; bars and forgings; design and production data, conversion
Edition 1992-08

Aerospace series - Weldable hardened and tempered chromium-molybdenum-vanadium steel, with approx. 0,15 C - 1,4 Cr - 0,9 Mo - 0,25 V - Part 1: Remelted with consumable electrode - Plate
Edition 2012-10

Aerospace series - Weldable hardened and tempered chromium-molybdenum-vanadium steel, with approx. 0,15 C - 1,4 Cr - 0,3 Mo - 0,25 V - Part 2: Remelted with consumable electrode - Bar and forging
Edition 2012-10

Aerospace series - Weldable hardened and tempered chromium-molybdenum-vanaduim steel with approx. 0,15 C - 1,4 Cr - 0,9 Mo - 0,25 V - Part 100: Consumable elektrode remelted - Plate, bar and forging - Design and production data, cross-referencing
Edition 2012-10

Aerospace; heat-resisting nickel alloy with approx. 0,1 C - 20 Cr - 2,3 Ti - 1,4 Al, consumable electrode remelted; sheet and strip
Edition 1993-08

Aerospace; heat-resisting nickel alloy with approx. 0,1 C - 20 Cr - 2,3 Ti - 1,4 Al, consumable electrode remelted; bars and forgings
Edition 1993-08

Aerospace; heat-resisting nickel alloy with approx. 0,1 C - 20 Cr - 18 Co - 2,5 Ti - 1,5 Al, consumable electrode remelted; sheet and strip
Edition 1993-08