Gold-Palladium-Nickel Alloy, Brazing Filler Metal, High Temperature 30Au - 34Pd - 36Ni 2075 to 2130 °F (1135 to 1166 °C) Solidus-Liquidus Range
- Aerospace Material Specification
- AMS4785G
- Cancelled
Scope
Rationale
Recommended Content
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Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | - Composition | |
TABLE 2 | - Standard Diameter Sizes | |
TABLE 3A | - Diameter Tolerances, Inch/Pound Units | |
TABLE 3B | - Diameter Tolerances, SI Units | |
TABLE 4 | - Standard Thicknesses | |
TABLE 5 | - Particle Size Distribution |
Issuing Committee
AMS F Corrosion and Heat Resistant Alloys Committee
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.