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SAE AMS4915

TITANIUM ALLOY SHEET, STRIP, AND PLATE 8Al – 1Mo - 1V Single Annealed

inactive
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Organization: SAE
Publication Date: 15 March 1966
Status: inactive
Page Count: 3
scope:

Application: Primarily for parts requiring strength up to 8000 F (427 C). where maximum fracture toughness is not critical.

Document History

June 1, 2017
Titanium Alloy Sheet, Strip, and Plate 8Al - 1V - 1Mo Single Annealed
Form This specification covers a titanium alloy in the form of sheet, strip, and plate up to 4.000 inches (101.60 mm), inclusive Application These products have been used typically for parts...
March 1, 2013
Titanium Alloy Sheet, Strip, and Plate 8Al - 1V - 1Mo Single Annealed
Form This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4.000 inches (101.60 mm). Application These products have been used typically for parts requiring...
December 1, 2008
Titanium Alloy Sheet, Strip, and Plate 8Al - 1V - 1Mo Single Annealed
Form This specification covers a titanium alloy in the form of sheet, strip, and plate. Application These products have been used typically for parts requiring strength up to 800 °F (427 °C) where...
August 1, 2003
Titanium Alloy Sheet, Strip, and Plate 8Al - 1V - 1Mo Single Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: These products have been used typically for parts requiring strength up to 800 °F (427 °C) where...
June 1, 2003
Titanium Alloy Sheet, Strip, and Plate 8Al - 1V - 1Mo Single Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: These products have been used typically for parts requiring strength up to 800 °F (427 °C) where...
July 1, 1990
Titanium Alloy Sheet, Strip, and Plate 8Al - 1V - 1Mo Single Annealed
SCOPE: Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: Primarily for parts requiring strength up to 800°F (427°C) where fracture toughness is not...
April 1, 1984
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8Al - 1V - 1Mo Single Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: Primarily for parts requiring strength up to 800°F (425°C) where fracture toughness is not...
July 15, 1977
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8Al - 1V - 1Mo Single Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Applications: Primarily of parts requiring strength up to 800°F (425°C) where fracture toughness is not...
January 15, 1977
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8Al - 1V - 1Mo Single Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: Primarily for parts requiring strength up to 800o F (425o C) where fracture toughness is not...
January 15, 1976
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8Al - 1V - 1Mo Single Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: Primarily for parts requiring strength up to 800 F (427° C) where fracture toughness is not...
November 1, 1968
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8Al – 1Mo- 1V Single Annealed
APPLICATION: Primarily for parts requiring strength up to 800 F (427 C) where maximum fracture toughness is not critical.
September 30, 1966
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8Al – 1Mo- 1V Single Annealed
APPLICATION: Primarily for parts requiring high strength up to 800 F (427 C) where maximum fracture toughness is not critical.
SAE AMS4915
March 15, 1966
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8Al – 1Mo - 1V Single Annealed
Application: Primarily for parts requiring strength up to 8000 F (427 C). where maximum fracture toughness is not critical.
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