Our fastening elements boast tensile strengths between 900 and 2100 MPa. Our standard materials include a range of high and low-alloy steels as well as titanium, nickel and cobalt-based alloys. We rely exclusively on sophisticated manufacturing processes such as hot forging, heat treatment and thread rolling. These processes ensure that our products have optimum mechanical and functional properties – to keep you safe. We have been specialising in the strictest standards and requirements for aerospace and space travel materials for many years. Let us know your special application needs – we’ll do everything we can to exceed even the most stringent requirements.
Standard materials overview:
Titanium alloys (TiAl6V4, TiBetaC)
High-strength, hardened and tempered steels (1.6604/E35NCD16/30NCD16/35CD4/1.7784)
Heat-resisting precipitation-hardening steels (A286/1.4944)
High-strength and corrosion-resistant steels (13-8 Mo/17-4 PH/15-5 PH/1.4534/1.4548/1.4545)
High-strength precipitation-hardening nickel alloys
Nimonic 80 A (2.4631)/Inconel 718 (2.4668)
High-strength and highly corrosion-resistant NiCo alloys
(MP159, MP35N)
Detailed descriptions are available here: