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TPF-C Technology Plan - Exoplanet Exploration Program - NASA

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Chapter 4<br />

Figure 4-5. Microslip Tribometer Characterization (MTC) apparatus.<br />

Figure 4-6 Representative data obtained from the Microslip Tribometer Characterization<br />

(MTC) facility.<br />

parasitic effects of cables through pivot or latch joints. Other areas of potential concern include<br />

micro-cracking and residual stress behavior of ULE segments joined through a low-temperature<br />

fusion process, especially as they relate to non-recoverable launch-induced deformations, or<br />

geometric misalignment of sub-assembly elements due to initial fabrication imperfections. This<br />

testbed could also be used to investigate active or passive structural damping technologies,<br />

should there be a need in the future. Details and test plans for the sub-assembly test articles will<br />

be developed as the design and analysis of <strong>TPF</strong>-C mature and as the understanding of these risks<br />

with respect to the error budget improve.<br />

The test facility will be multi-functional and will be capable of measuring nm-level motions due<br />

to thermal or mechanical disturbances. Tests will range from long-term stability observations to<br />

high frequency measurements, all of which are required to investigate a variety of nonlinear<br />

mechanical physics. For instance, test articles will be tested for quasi-static thermal or<br />

mechanical cyclic loads to identify hysteresis, and for steady-state dynamic loads to characterize<br />

harmonic distortion of the frequency response. When testing hinge and latch assemblies, the<br />

specimens will be turned around in various orientations to investigate and model the effects of 0-<br />

gravity. Alternatively, means to artificially change the pre-load on the frictional interfaces will<br />

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