Analysis of the possibility of using the system for small satellite de-orbiting based on an aerodyna...
Analysis of the possibility of using the system for small satellite de-orbiting based on an aerodynamic stabilizer, taking into account the physical features of the Earth's upper atmosphere
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Publisher
Bristol: IOP Publishing
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Language
English
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Publisher
Bristol: IOP Publishing
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Scope and Contents
Contents
The paper presents an analysis of performance of a satellite de-orbiting system that utilizes a deployable aerodynamic stabilizer for controling the angular motion of a spacecraft in order to ensure the correct orientation of the breaking impulse. The problem of determining the shape of the stabilizer, considering its performance requirements and t...
Alternative Titles
Full title
Analysis of the possibility of using the system for small satellite de-orbiting based on an aerodynamic stabilizer, taking into account the physical features of the Earth's upper atmosphere
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TN_cdi_proquest_journals_2566209964
Permalink
https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_proquest_journals_2566209964
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ISSN
1742-6588
E-ISSN
1742-6596
DOI
10.1088/1742-6596/1236/1/012087
