Modeling the shape correction of a thin-walled composite reflector of a spacecraft
This paper examines an adjustable thin-wall composite reflector for a small satellite. The reflector consisted of 6 identical sectors which had 4 adjusting units in the form of linear actuators. The purpose of this work was to explore the capabilities of numerical modeling to ensure the shape correc...
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| Main Author: | |
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| Format: | Article |
| Language: | Russian |
| Published: |
Association «Technology Platform «National Information Satellite System»
2024-01-01
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| Series: | Космические аппараты и технологии |
| Subjects: | |
| Online Access: | http://journal-niss.ru/journal/archive/48/paper5.pdf |
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