Paper
23 October 1995 Ultralightweight off-axis three-mirror anastigmatic SiC visible telescope
Joseph L. Robichaud, Michael I. Anapol, Leo R. Gardner, Peter Hadfield
Author Affiliations +
Abstract
The next generation of space-borne optical sensor will have to meet tight weight limitation, in order to be viable on smaller, less expensive, launch platforms, while supporting a wide range of mission scenarios. Wide spectral coverage, near-diffraction limited visible quality performance, and increased thermal and structural stability are becoming important features for future space-hardware. SiC represents an emerging technology which is gaining wider acceptance as the leading candidate for the next generation of space flight hardware. As a material for all-reflective flight telescopes and optical benches, SiC offers: the lightweight and stiffness characteristics of beryllium; glass-like inherent stability consistent with visible quality performance levels; superior thermal properties down to cryogenic temperatures and in the presence of large thermal gradients; and an existing, commercially based material and processing infrastructure like aluminum. This paper describes an all-SiC off-axis, three mirror anastigmatic telescope system which promises to meet these stressing technical requirements. The system described maintains a 35 cm entrance aperture with a weight of 14 kgs.
© (1995) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Joseph L. Robichaud, Michael I. Anapol, Leo R. Gardner, and Peter Hadfield "Ultralightweight off-axis three-mirror anastigmatic SiC visible telescope", Proc. SPIE 2543, Silicon Carbide Materials for Optics and Precision Structures, (23 October 1995); https://doi.org/10.1117/12.225287
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CITATIONS
Cited by 5 scholarly publications.
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KEYWORDS
Silicon carbide

Space telescopes

Mirrors

Telescopes

Aluminum

Sensors

Beryllium

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