TPF-C Technology Plan - Exoplanet Exploration Program - NASA
TPF-C Technology Plan - Exoplanet Exploration Program - NASA
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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