MODELING OF THE TEMPERATURE AND STRESSED-STRAINED STATES OF THE REFLECTOR OF A MIRROR SPACE ANTENNA

Results of modeling of the temperature and stressed-strained states of the refl ector of a mirror space antenna installed on a spacecraft that conducts a fl ight on geostationary and low near-earth orbits have been presented.
   
Author:  S. V. Reznik, P. V. Prosuntsov, and A. V. Azarov
Keywords:  reflector, mirror space antenna, spacecraft, geostationary and low near-earth orbits
Page:  978