Control system of the radio-reflective surface shape of a large-size space reflector using its current-conducting structural parts-Reference-Cited by-同舟云学术

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Control system of the radio-reflective surface shape of a large-size space reflector using its current-conducting structural parts

Published:2024-06 Issue: Volume:219 Page:592-602
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Mitin F.V.^ORCID,Shirshov A.D.,Konoplev Y.V.^ORCID,Yuev A.A.^ORCID,Krivushov A.I.^ORCID

Funder

Russian Science Foundation

Publisher

Elsevier BV

Reference28 articles.

1. Gossamer spacecraft;Chmielewski,2005

2. 30 m class lightweight large deployable reflector;Ozawa,2011

3. Pretension design for space deployable mesh Reflectors under multi-uncertainty;Hanqing;Acta Astronaut.,2015

4. Design of geodesic cable net for space deployable mesh reflectors;Hanqing;Acta Astronaut.,2016

5. Design and performance of Astromesh reflector onboard Soil moisture active passive spacecraft;Mobrem,2012

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