Development of structural-composite reflector panels for a submillimeter space telescopeReflector 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.
Document ID
19860013141
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Freeland, R. E. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 12, 2013
Publication Date
November 1, 1985
Publication Information
Publication: ESA Proceedings of 3rd European Symposium on Spacecraft Materials in Space Environment