Paper
29 July 2016 CFRP mirror technology for cryogenic space interferometry: review and progress to date
Martyn L. Jones, David Walker, David A. Naylor, Ian T. Veenendaal, Brad G. Gom
Author Affiliations +
Abstract
The FP7 project, FISICA (Far Infrared Space Interferometer Critical Assessment), called for the investigation into the suitability of Carbon fiber Reinforced Plastic (CFRP) for a 2m primary mirror. In this paper, we focus on the major challenge for application, the development of a mirror design that would maintain its form at cryogenic temperatures. In order to limit self-emission the primary is to be cooled to 4K whilst not exceeding a form error of 275nm PV. We then describe the development of an FEA model that utilizes test data obtained from a cryogenic test undertaken at the University of Lethbridge on CFRP samples. To conclude, suggestions are made in order to advance this technology to be suitable for such an application in order to exploit the low density and superior specific properties of polymeric composites.
© (2016) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Martyn L. Jones, David Walker, David A. Naylor, Ian T. Veenendaal, and Brad G. Gom "CFRP mirror technology for cryogenic space interferometry: review and progress to date", Proc. SPIE 9904, Space Telescopes and Instrumentation 2016: Optical, Infrared, and Millimeter Wave, 99046F (29 July 2016); https://doi.org/10.1117/12.2233645
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Cited by 1 scholarly publication.
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KEYWORDS
Mirrors

Mirrors

Cryogenics

Space telescopes

Space telescopes

Telescopes

Telescopes

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