Nickel Alloy, Brazing Filler Metal 71Ni - 10Si - 19Cr 1975 °F (1080 °C) Solidus, 2075 °F (1135 °C) Liquidus
- Aerospace Material Specification
|Aerospace Material Specification||Nickel Alloy, Brazing Filler Metal 94Ni - 3.5Si - 1.8B 1800 °F (982 °C) Solidus, 1950 °F (1066 °C) Liquidus|
|Aerospace Material Specification||Nickel Alloy, Brazing Filler Metal 92Ni - 4.5Si - 3.1B 1800 to 1900 °F Solidus-Liquidus Range|
|Aerospace Material Specification||Cobalt Alloy, High Temperature Brazing Filler Metal 50Co - 8.0Si - 19Cr - 17Ni - 4.0W - 0.80B 2050 to 2100 °F (1121 to 1149 °C) Solidus-Liquidus Range|
Data Sets - Support Documents
|[Unnamed Dataset 1]|
The committee of Corrosion and Heat Resistant Steels and Alloys and Specialty Steels and Alloys, AMS Committee F, will prepare, coordinate, and revise documents related to corrosion and heat resistant steels and alloys and specialty steels and alloys technology, such as stainless steels and nickel and base alloys, through the participation of metals suppliers, users, and interested government agencies. Committee activities shall provide a forum for the cooperative interchange of ideas and experience of the participants, resulting in the publication of specifications that embody sound, established aerospace industry practices and requirements to serve the suppliers and customers of aerospace materials.