Publication Date:
2019-08-28
Description:
The stress informed state of the mirror of an antenna, with a diameter of 3 m, for a radio interferometer used in space, and located in a temperature field is examined. The mirror represents a parabolic shell, consisting of 19 identical parts. The problem is based on representations of the thermoelasticity of thin shells.
Keywords:
OPTICS
Type:
NASA-TM-75633
,
PR-412
Format:
application/pdf
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