DETERMINATION OF LOADS FOR STRENGTH CALCULATIONS OF THE ATTACHMENT FITTINGS OF THE DEVICES AND ASSEMBLIES OF A SPACECRAFT IN A POWERED FLIGHT - PDF (Russian)
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Keywords
acoustic emission
aluminum
competence
corrosion
corrosion resistance
electrical conductivity
fractography
grinding
heat treatment
magnesium alloys
mathematical model
mechanical properties
microhardness
microstructure
modeling
nanoparticles
plastic deformation
professional competence
roughness
strength
structure
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Keywords
acoustic emission
aluminum
competence
corrosion
corrosion resistance
electrical conductivity
fractography
grinding
heat treatment
magnesium alloys
mathematical model
mechanical properties
microhardness
microstructure
modeling
nanoparticles
plastic deformation
professional competence
roughness
strength
structure
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