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Space mirror deformation: from thermo-mechanical measurements by speckle interferometry to optical comparison with
This study validates a multiphysics modeling tool for predicting space optic performance under thermal loads. The simulation accurately predicts mirror surface deformations, reducing the need for costly physical testing.
Area of Science:
- Optical engineering
- Materials science
- Computational physics
Background:
- Space optics require rigorous experimental testing for performance validation.
- Increasingly stringent optical requirements make these tests expensive and time-consuming.
- A predictive modeling tool can mitigate these challenges.
Purpose of the Study:
- To develop and validate a multiphysics modeling approach for space optics.
- To predict the behavior of space optics under thermal loads.
- To compare experimental and simulation results for thermal deformation and wavefront error.
Main Methods:
- A multiphysics approach was employed to simulate optic behavior under thermal stress.
- Electronic speckle pattern interferometry (ESPI) measured local surface displacements.
- Rigid body motion was subtracted to determine surface deformation.
- Thermo-mechanical simulation results were validated against experimental data.
Main Results:
- Experimental surface deformations of a space mirror under thermal gradients were accurately predicted by the multiphysics model.
- The validated thermo-mechanical solution showed good agreement between experimental and numerical wavefront errors.
- The modeling tool offers a viable alternative to extensive physical testing.
Conclusions:
- The multiphysics modeling approach is effective for predicting space optic performance under thermal loads.
- This simulation tool can significantly reduce the cost and time associated with experimental testing.
- The validated model provides a reliable method for assessing optical performance in realistic conditions.
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