SUBSTANTIATION OF THE STRUCTURAL-LAYOUT SCHEME OF THE MIRROR-SPACE-ANTENNA REFLECTOR WITH A HIGH SHAPE STABILITY AND A LOW DENSITY PER UNIT LENGTH

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SUBSTANTIATION OF THE STRUCTURAL-LAYOUT SCHEME OF THE MIRROR-SPACE-ANTENNA REFLECTOR WITH A HIGH SHAPE STABILITY AND A LOW DENSITY PER UNIT LENGTH

Volume 88, №3

SUBSTANTIATION OF THE STRUCTURAL-LAYOUT SCHEME OF THE MIRROR-SPACE-ANTENNA REFLECTOR WITH A HIGH SHAPE STABILITY AND A LOW DENSITY PER UNIT LENGTH

Problems of designing space-antenna reflectors from composite materials for promising telecommunication satellites are considered. Selection of designs is based on the numerical modeling of heat-transfer and mechanics processes corresponding to orbital-fl ight conditions

Author: S. V. Reznik, P. V. Prosuntsov, and A. V. Azarov
Keywords: spacecraft, mirror antennas, reflectors, composite materials.
Page: 699

Link

S. V. Reznik, P. V. Prosuntsov, and A. V. Azarov. SUBSTANTIATION OF THE STRUCTURAL-LAYOUT SCHEME OF THE MIRROR-SPACE-ANTENNA REFLECTOR WITH A HIGH SHAPE STABILITY AND A LOW DENSITY PER UNIT LENGTH //Journal of engineering physics and thermophysics. №3. Volume 88, №3. P. 699.

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