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satellite structures

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Journal Articles
Alloy Digest (1987) 36 (5): Be-4.
Published: 01 May 1987
... BRUSH WELLMAN S-200F is beryllium strengthened by a dispersion of beryllium oxide (1.5%). It has moderate strength and moderate ductility (A minumum of 2.0% elongation). Its uses include optical equipment, nuclear reactors, instrumentation, optical substrates, satellite structures and solar arrays...
Journal Articles
Alloy Digest (1987) 36 (7): Be-5.
Published: 01 July 1987
... BRUSH WELLMAN SR-200E is a grade of beryllium strengthened by a dispersion of beryllium oxide (2.0%). It has relatively high strength and ductility (a minimum of 10% elongation). Its uses include missiles, space vehicles, structural parts on both commercial and military satellites and optical...
Journal Articles
Alloy Digest (1987) 36 (1): Be-3.
Published: 01 January 1987
... parts and (7) Satellite structures (truss tubes. antenna booms, skin materials and solar arrays). Manufacturer: Brush Wellman Inc. Cleveland, Ohio 44110. ...
Journal Articles
Alloy Digest (1964) 13 (2): Mg-56.
Published: 01 February 1964
... Characteri sties: Magnesiun LA141A is a magnesium-lithium alloy having rbe lightest weight of all structural metals. For satellite payload structures and spacecraft, ir offers distinct and valuable weight advantages. In gauges under one inch, ic has proved co be effective as armor plate. It absorbs energy...
Journal Articles
Alloy Digest (1997) 46 (9): Be-9.
Published: 01 September 1997
... Beralcast 363, 191, and 310 are lightweight beryllium-aluminum (Be-Al) alloys for producing near net shapes by investment casting. Beralcast 363 is used primarily for structural applications, Beralcast 191 is used primarily for electronic packaging and Beralcast 310 for wrought products (from cast...
Journal Articles
Alloy Digest (1965) 14 (7): Mg-58.
Published: 01 July 1965
... Magnesium-LA91 is a magnesium-lithium lightweight alloy recommended for missile and space vehicle structures. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well...
Journal Articles
Alloy Digest (1971) 20 (9): Be-1.
Published: 01 September 1971
... in satellites, space probes and rockets. Forms Available: Rod, bar, tubes, angles and sheet Applications: Box beams, open spaceframe structures, control shafts and tubes, extendable solar frames and arresting gear, bulkhead stiffeners, torque tubes, actuating rods, framing members. Manufacturer: Kawecki Berylco...
Journal Articles
Alloy Digest (2007) 56 (2): Fe-140.
Published: 01 February 2007
.... This is particularly so in the case of hydrogen and cracked ammonia. Variations in the modulus of elasticity as a function of temperature are indistinguishable from those of other alloys. Durimphy does not undergo any structural change down to the lowest temperatures and does not exhibit any particular cold...
Journal Articles
Alloy Digest (2007) 56 (3): Fe-141.
Published: 01 March 2007
... alloys. Phytime does not undergo any structural change down to the lowest temperatures and does not exhibit any particular cold brittleness. Weldability: Phytime welds well using electric spot welding, electron beam weld- ing, and with argon arc welding (generally tungsten inert gas, or TIG). Phytime can...
Journal Articles
Alloy Digest (2021) 70 (1): Ti-174.
Published: 01 January 2021
... using the proprietary plasma atomization pro- cess. This alloy powder is a spherical powder with virtually Melting range °C 1538 1649 no entrapped porosity and few satellites. The particle size (°F) (2800 3000) is between 45 and 100 µm (1770 and 3935 µin The limit on the minimum particle size ensures...
Journal Articles
Alloy Digest (2021) 70 (9): Ni-775.
Published: 01 September 2021
... (1 Ni 36 (1.3912) in.) of maximum section thickness. Cool in still air. Compared to cooling in air, cooling in water results in a lower coefficient General Characteristics of linear thermal expansion. However, the resulting micro- structure is not stable. If the extent of deformation following...