| Issue |
MATEC Web Conf.
Volume 110, 2017
International Youth Scientific Conference “Heat and Mass Transfer in the Thermal Control System of Technical and Technological Energy Equipment” (HMTTSC 2017)
|
|
|---|---|---|
| Article Number | 01072 | |
| Number of page(s) | 4 | |
| DOI | https://doi.org/10.1051/matecconf/201711001072 | |
| Published online | 19 June 2017 | |
Comparison of space antennas mirror reflectors parameters made of composite materials
Bauman Moscow State Technical University, 105005 Moscow, Russia
* Corresponding author: sreznik@bmstu.ru
Communication satellites today are fitted with one or more parabolic antenna reflectors. The unique mechanical and thermal characteristics mean that space antenna reflectors (AR) are most frequently fabricated from carbon-fibre reinforced plastics (CFRP). The reflector design must meet the stringent requirements for low linear density and high dimensional stability.
© The Authors, published by EDP Sciences, 2017
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