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NASA NTRS · 19760009074

Laser space rendezvous and docking system trade-off study

Abstract

The use, design, and fabrication feasibility of scanning the laser beam by swiveling the outside mirror with a ball joint swivel system is examined along with the applicability of graphite reinforced epoxy material for the construction of reflective optics. It is indicated that (1) the cost of graphite-epoxy will be more than that of many other materials due to the amount of special tooling required; (2) the weight advantage of graphite-epoxy over beryllium is minimal; the ball joint swivel system is accurate enough to perform the scanning function; and that the ball joint will result in a simpler and more cost effective scanning mechanism.

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BibTeXRIS

Adelman, S., Levinson, S.. 1975-12-01. Laser space rendezvous and docking system trade-off study. https://ntrs.nasa.gov/citations/19760009074

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