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Author : J. L. Ratliff,H. R. Ogden
Publisher : Unknown
Page : 32 pages
File Size : 47,5 Mb
Release : 1962
Category : Heat resistant alloys
ISBN : UOM:39015095154996
Author : Anonim
Publisher : Unknown
Page : 426 pages
File Size : 46,5 Mb
Release : 1962
Category : Science
ISBN : OSU:32435052247517
Author : F. F. Schmidt,Battelle Memorial Institute. Defense Metals Information Center
Publisher : Unknown
Page : 154 pages
File Size : 40,8 Mb
Release : 1963
Category : Tungsten
ISBN : UOM:39015095154657
The results of a state-of-the-art survey covering tungsten and ten of its alloys are presented. All data are given in tabular and graphical form covering some of the more important physical, mechanical, and metallurgical properties for each material. References are given at the conclusion of each material section.
Author : Paul F. Sikora,Robert W. Hall
Publisher : Unknown
Page : 20 pages
File Size : 40,9 Mb
Release : 1959
Category : Aerospace engineering
ISBN : UIUC:30112106741777
Author : R. H. Ernst,D. N. Williams,H. R. Ogden
Publisher : Unknown
Page : 12 pages
File Size : 50,8 Mb
Release : 1964
Category : Titanium
ISBN : UOM:39015095155613
A brief study of delayed fracture in a seam-welded titanium panel is summarized in this memorandum. Examination of the fracture surface with electron microscopy showed that the material cleaved, failing in a brittle manner. Although the nature of the embrittlement was not clearly defined, titanium hydride phase was suspected as a prime contributor to failure. Even though the hydrogen content of the titanium was only 65 ppm, hydride embrittlement was thought to have occurred from precipitation of hydride platelets on crystal planes oriented normal to welding stresses. Other work, briefly discussed in the memorandum, has confirmed that hydride platelets in titanium can be oriented by stress and that tensile ductility of Zircaloy (which behaves similarly with respect to hydrogen, to titanium) depends upon hydride orientation. Stress-relief annealing of welded titanium structures is recommended wherever possible to minimize embrittlement by stress-oriented hydrides. (Author).
Author : Anonim
Publisher : Unknown
Page : 54 pages
File Size : 52,6 Mb
Release : 1964
Category : Electronic
ISBN : UOM:39015095155639
To aid in quick identification and easy location of specific technical data and information in the various reports and memoranda which have been prepared and distributed by the Defense Metals Information Center, as well as by DMIC's forerunner, the Titanium Metallurgical Laboratory, a classification by major subject matter was prepared. The classification covers reports through DMIC Report 193 and memoranda through DMIC Memorandum 183. (Author).
Author : Battelle Memorial Institute. Defense Metals Information Center
Publisher : Unknown
Page : 38 pages
File Size : 54,7 Mb
Release : 1968
Category : Alloys
ISBN : UOM:39015095158161
Author : Anonim
Publisher : Unknown
Page : 764 pages
File Size : 45,5 Mb
Release : 1975
Category : Nuclear energy
ISBN : UOM:39015023546412
Author : John David Jackson,Walter K. Boyd,Paul D. Miller
Publisher : Unknown
Page : 32 pages
File Size : 46,5 Mb
Release : 1963
Category : Liquid oxygen
ISBN : UOM:39015095155571
Author : W. S. Hyler,Robert Melvin Evans
Publisher : Unknown
Page : 36 pages
File Size : 45,6 Mb
Release : 1962
Category : Heat resistant alloys
ISBN : UOM:39015095155142
Author : Albert M. Hall
Publisher : Unknown
Page : 30 pages
File Size : 49,9 Mb
Release : 1962
Category : Maraging steel
ISBN : UOM:39015095155720
Author : F. J. Barone,Albert M. Hall
Publisher : Unknown
Page : 38 pages
File Size : 45,9 Mb
Release : 1963
Category : Stainless steel
ISBN : UOM:39015095155423
Author : M. S. Farkas
Publisher : Unknown
Page : 30 pages
File Size : 53,9 Mb
Release : 1963
Category : Uranium
ISBN : UOM:39015095155712
Author : C. H. Lund,H. J. Wagner
Publisher : Unknown
Page : 32 pages
File Size : 49,6 Mb
Release : 1962
Category : Heat resistant alloys
ISBN : UOM:39015095154988
Author : R. L. Pasley,C. L. Seale
Publisher : Unknown
Page : 20 pages
File Size : 53,5 Mb
Release : 1962
Category : Solid propellant rocket engines
ISBN : UOM:39015095155290
Methods are given for nondestructively inspecting rocket motor cases, nozzles, and motor-case insulation. The motor cases may be fabricated from steel, titanium, or glass-reinforced plastics and made by welding or wrapping processes. In some designs, the nozzle consists of tungsten inserts fitted in graphite heat-sink backup rings with a molybdenum sleeve shrunk over the graphite ring. The inside insulation is generally a rubber-base substance adhered to the motor case. (Author).