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Standard
1952-06-01
This specification covers requirements for identification of forgings, including die forgings, hand forgings, and rolled rings.
Technical Paper
1952-01-01
Frank Watson
Standard
1951-12-01
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of December 2008. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been "CANCELLED ".
Standard
1951-12-01
This specification covers the engineering requirements for finishng aircraft parts and assemblies with an engine gray enamel.
Standard
1951-10-01
This specification covers the engineering requirements for producing a thin tin coating on aluminum alloys by an immersion process.
Standard
1951-10-01
This specification covers the procedure to be used for spraying metallic parts with aluminum and the properties of the coating.
Standard
1951-10-01
This specification covers the engineering requirements for finishing aircraft parts and assemblies with a black enamel.
Standard
1951-10-01
This specification covers the requirements for electrodeposed lead on metal part.
Standard
1951-10-01
This specification covers the engineering requirements for electrodeposition of silver on other metals, usually with a nickel strike between the basis metal and the silver.
Standard
1951-10-01
This specification covers the requirements for electrodeposited zinc plating. Unless otherwise stated on the engineering drawing, high strength steel parts having a hardness of 45 HRC or greater shall not be electroplated.
Standard
1951-10-01
This specification covers the requirements for a manganese phosphate coating on ferrous alloys.
Standard
1951-10-01
This specification covers the requirements for electrodeposited and diffused lead and indium plate.
Standard
1951-10-01
This specification covers the requirements for identification of finished parts.
Standard
1951-10-01
This specification covers the requirements for silver deposited on metal parts with a copper strike between the basis metal and the silver deposit. This process has been used typically to provide a bearing surface and to prevent galling or seizing of metal surfaces of parts made of materials where a high baking temperature may be detrimental to the properties of the basis material.
Standard
1951-10-01
This specification covers the requirements for black oxide coatings on parts.
Standard
1951-10-01
This specification covers the requirements for electrodeposited cadmium on metal parts.
Standard
1951-10-01
This specification covers the engineering requirements for electrodeposition of nickel and the properties of the deposit.
Standard
1951-10-01
This specification covers the requirements for electrodeposited copper.
Standard
1951-10-01
This specification covers the engineering requirements for automatic peening of surfaces of parts by impingement of metallic shot, glass beads, or ceramic shot. To induce residual compressive stress in surface layers of parts, thereby increasing fatigue strength and resistance to stress-corrosion cracking but usage is not limited to such applications.
Standard
1951-06-01
This specification covers the engineering requirements for electrodeposition of a porous chromium plate and the properties of the deposit.
Standard
1951-06-01
This specification covers established inch/pound manufacturing tolerances applicable to low-alloy steel bars ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "exclusive " is used to apply only to the higher figure of the specified range.
Technical Paper
1951-01-01
W. S. SAVILLE
Standard
1950-12-01
This specification covers established inch/pound manufacturing tolerances applicable to low-alloy steel bars ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "exclusive " is used to apply only to the higher figure of the specified range.
Standard
1950-06-01
This specification covers the requirements for producing a zinc phosphate coating on ferrous alloys and the properties of the coating. This process has been used typically to produce a coating that will ensure satisfactory paint adherence, but usage is not limited to such applications.
Standard
1950-06-01
This specification has been declared 'CANCELLED' by the Aerospace Materials Division SAE, as of April 1996. and has been superseded ASTM E 1444.
Standard
1950-06-01
This specification covers the engineering requirements for producing brazed joints using copper as the brazing filler metal.
Standard
1950-06-01
This specification covers the engineering requirements for producing brazed joints in parts fabricated from steels, iron alloys, nickel alloys, cobalt alloys, and copper alloys by use of silver alloys, and the properties of such joints. This procedure has been used typically for joints requiring high strength up to 400 degrees F (204 degrees C), but usage is not limited to such applications.
Magazine
1950-04-01
Viewing 3181 to 3210 of 3305

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