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Viewing 164041 to 164070 of 175566
1961-01-01
Technical Paper
610462
Capt. R. S. Stewart
1961-01-01
Technical Paper
610465
Michael C. Kaye
1961-01-01
Technical Paper
610464
V. L. Larrowe, M. M. Spencer
1961-01-01
Technical Paper
610460
D. D. Dankel
1961-01-01
Technical Paper
610467
Henry Dreyfuss
1961-01-01
Technical Paper
610469
O. S. Carliss
1961-01-01
Technical Paper
610468
John Gale, G. T. Scharfenberg, J. N. Polivka
1961-01-01
Technical Paper
610471
F. W. Newburgh, B. Ingold
1961-01-01
Technical Paper
610473
R. K. Reynolds, E. Mayer
1961-01-01
Technical Paper
610472
Turner G. Timberlake
1961-01-01
Technical Paper
610475
E. H. Fletcher
1961-01-01
Technical Paper
610474
David F. Morgan
1961-01-01
Standard
AMS4912B
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of December, 1991.
1961-01-01
Standard
AMS5359
This specification covers a corrosion and heat resistant steel in the form of sand castings.
1961-01-01
Standard
AMS5368
This specification covers a corrosion-resistant steel in the form of investment castings.
1961-01-01
Standard
AMS5753
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, and stock for forging or heading. Primarily for parts, such as turbine blades, bolts, and fittings, requiring high strength up to 1600 degrees F (870 degrees Centigrade) and oxidation resistance up to 1800 degrees F (980 degrees C). This specification has been declared "Noncurrent" by the Aerospace materials Division, SAE, as of October 16, 1987. It is recommended, therefore, that this specification not be specified for new designs.
1961-01-01
Standard
AMS5573C
This specification covers a corrosion and heat-resistant steel in the form of seamless tubing.
1961-01-01
Standard
AMS5812
This specification covers a corrosion and heat resistant steel in the form of welding wire. This wire has been used typically as bare wire filler metal for gas-tungsten-arc or gas-metal-arc welding of critical weldments of precipitation-hardenable, corrosion and heat resistant steels of similar composition where the weld area is required to have comparable strength and corrosion resistance to that of the parent metal, but usage is not limited to such applications.
1961-01-01
Standard
AMS3366
null, null
This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of February 22, 1989. It is recommended, therefore, that this specification not be specified for new designs.
1961-01-01
Standard
AMS3365
null, null
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of June, 1996.
1961-01-01
Standard
AMS3344
This specification has been "Cancelled" by the Aerospace Materials Division, SAE, as of January 1997.
1961-01-01
Standard
AMS4036
This specification covers an aluminum alloy in the form of sheet and plate clad on one side with a different aluminum alloy.
1961-01-01
Standard
AMS4058A
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
1961-01-01
Standard
AMS4057A
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
1961-01-01
Standard
AMS3870
This specification covers dense, ultra-high alumina in the form of moldings and extrusions.
1961-01-01
Standard
AMS7901A
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October, 1992.
1961-01-01
Standard
AMS7900A
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October, 1992.

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