Hi,

If you use aluminum 6082 alloy in a component for the satellite where the temperature can fluctuate from 180 to -160 C. Would the yield strength decrease over a period of 15 years in space?

Also, would the Elastic Limit change, if say the material is under compression of 200 MPa and deforms elastically at 0.2mm? Could this property change over the 15 year period due to temperature?

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