THERMAL STABILITY OF REFRACTORY METAL ALLOYS. [electronic resource]
C-129y (niobium Alloy)/stability And Tensile Properties At High Temperatures, Evaluation For Space System Use; Fs-85 (niobium Alloy)/stability And Tensile Properties At High Temperatures, Evaluation For Space System Use; Scb- 291 (niobium Alloy)/stability And Tensile Properties At High Temperatures,...
Saved in:
| Online Access: |
Online Access |
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| Corporate Author: | |
| Format: | Government Document Electronic eBook |
| Language: | English |
| Published: |
Washington, D.C : Oak Ridge, Tenn. :
United States. Dept. of Energy ; distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy,
1970.
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| Subjects: |
MARC
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| 245 | 0 | 0 | |a THERMAL STABILITY OF REFRACTORY METAL ALLOYS. |h [electronic resource] |
| 260 | |a Washington, D.C : |b United States. Dept. of Energy ; |a Oak Ridge, Tenn. : |b distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy, |c 1970. | ||
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| 500 | |a 01/01/1970. | ||
| 500 | |a "nasa-sp--245" | ||
| 500 | |a Gold, R.E.; Lessmann, G.G. | ||
| 500 | |a Westinghouse Electric Corp., Pittsburgh, Pa. Astronuclear Lab. | ||
| 520 | 0 | |a C-129y (niobium Alloy)/stability And Tensile Properties At High Temperatures, Evaluation For Space System Use; Fs-85 (niobium Alloy)/stability And Tensile Properties At High Temperatures, Evaluation For Space System Use; Scb- 291 (niobium Alloy)/stability And Tensile Properties At High Temperatures, Evaluation For Space System Use; T-222 (tantalum Alloy)/stability And Tensile Properties At High Temperatures, Evaluation For Space System Use; Tungsten Alloys And Systems/ta-base--w, Stability And Tensile Properties At High Temperatures, Evaluation For Space System Use; Nesdps Office Of Nuclear Energy Space And Defense Power Systems; D-43 (niobium Alloy)/stability And Tensile Properties At High Temperatures, Ev; B-66 (niobium Alloy)/ Stability And Tensile Properties At High Temperatures, Evaluation For Space System Use; Cb-752 (niobium Alloy)/stability And Tensile Properties At High Temperatures, Evaluation For Space System Use; Tantalum Alloys And Systems/ta-base--w, Stability And Tensile Properties At High Temperatures, Evaluation For Space System Use. | |
| 650 | 7 | |a Niobium Alloys-- Tungsten Alloys-- Zirconium Alloys. |2 local. | |
| 650 | 7 | |a High Temperature-- Space-- Stability-- Tensile Properties-- Uses. |2 local. | |
| 650 | 7 | |a Tantalum Alloys-- Tungsten Alloys. |2 local. | |
| 650 | 7 | |a Molybdenum Alloys-- Niobium Alloys-- Vanadium Alloys-- Zirconium Alloys. |2 local. | |
| 650 | 7 | |a Hafnium Alloys-- Niobium Alloys-- Tungsten Alloys-- Yttrium Alloys. |2 local. | |
| 650 | 7 | |a Tantalum Alloy T-111. |2 local. | |
| 650 | 7 | |a Niobium Alloys-- Tantalum Alloys-- Tungsten Alloys. |2 local. | |
| 650 | 7 | |a Carbides-- Niobium Alloys-- Tungsten Alloys-- Zirconium Alloys. |2 local. | |
| 650 | 7 | |a Tantalum Alloy-t222. |2 local. | |
| 650 | 7 | |a Niobium Alloys-- Tantalum Alloys-- Tungsten Alloys-- Zirconium Alloys. |2 local. | |
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