The MIRI instrument on the James Webb Space Telescope is equipped with detectors which are susceptible to signal disruption by the charge deposited from impacting cosmic rays. In order to quantify the degree to which the structure of MIRI will shield the detectors, we have used an opto-mechanical ray tracing approach, whereby the solid bodies in a detailed 3D model of the instrument are substituted with an absorptive glassy material. By importing this modified model into a ray tracing program (Tracepro) and then launching many rays from the detector, we have been able to generate a map of aluminium path length as a function of direction. We find that there is a minimum thickness of 2 to 3 mm over a few patches which subtend no more than 1.5 % of the sky for the worst case, imager detector. We discuss the performance of the shielding provided by the MIRI structure, concluding that this minimum thickness of aluminium is sufficient to suppress the impact of low energy protons below the level of the unavoidable flux due to high energy cosmic rays.
Largely thermal considerations have led the James Webb Space Telescope (JWST) Mid Infra Red Instrument (MIRI) European Consortium to specify a CFRP hexapod with rigidised Invar endfittings and brackets to form the Primary Structure of the instrument. Each bracket incorporates a pair of orthogonal flexures to provide kinematic mounting to JWST.
The principal alignment of the instrument, namely the placing of the Pick-off Mirror (POM) in the telescope frame, must be known and be trackable by a combination of measurement and prediction. Contributors to the alignment are many and various, but potentially great uncertainty lies with the use of a hexapod with field separable joints. In order to provide continuous measurement of the response of the Primary Structure hexapod to integration, g release effects and
thermoelastic effects, we have installed a strain gauge array in proximity to the flexures. In this way, asymmetrical strains, inadvertantly introduced during integration, may be detected. The technology employed is that of optical Fibre Bragg Gratings (FBGs), which allow us to measure strains continuously from room temperature down to cryogenic temperatures, with a modest investment in temperature calibration. The strain array has been used during the integration and testing of the Structural Thermal Model of the instrument, and some data have been obtained regarding the utility
and effectiveness of this technique in diagnosing sources of alignment error buildup. This paper describes the technology employed, the logic behind these measurements and experience with integration and calibration. Analysis, and the results of some tests, both mechanical and thermal, are presented and discussed.
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