1 July 1990 Design of a shuttle-based space debris telescope
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A 1.6-meter diameter f/0.95 all-reflecting telescope was designed to observe orbital debris particles as small as 1 mm from the shuttle payload bay. The telescope was specified to have a flat focal surface without the imposition of refractive elements. Two design configurations involving three mirrors were evaluated - a reflective Schmidt-Cassegrain and a modified Paul corrector. The Paul system was found to be more compact and appropriate for this application.
© (1990) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Eric Harvey Richardson, Eric Harvey Richardson, David L. Talent, David L. Talent, Constance L. Tritsch, Constance L. Tritsch, Faith Vilas, Faith Vilas, } "Design of a shuttle-based space debris telescope", Proc. SPIE 1236, Advanced Technology Optical Telescopes IV, (1 July 1990); doi: 10.1117/12.19202; https://doi.org/10.1117/12.19202


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