NASA NTRS ยท 19860013141
Development of structural-composite reflector panels for a submillimeter space telescope
Abstract
Reflector panels for the Large Deployable Reflector (LDR) for a 20m, Earth-orbiting, submillimeter and infrared telescope were designed. The panels must be 1 to 2 m in diameter with surface precision and thermal stability of a few microns, and an areal density of or = 10 kg/sqm. Using a combination of design, analytical modeling, panel fabrication, and testing, two sizes of graphite/epoxy panels were produced. One is 15 sqcm the other 60 sqcm, both weighing 5 to 7 kg/sqm with manufactured surface accuracies of a few tenths of a micron and thermal stability at LDR orbital temperatures of a few microns.
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Freeland, R. E.. 1985-11-01. Development of structural-composite reflector panels for a submillimeter space telescope. https://ntrs.nasa.gov/citations/19860013141
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