Development of small-scale autorotative lander for ISS payload
This paper considers the development of a small descent vehicle (SA) and technology for its descent using the autorotation effect for braking in the atmosphere. The tasks that need to be solved in the process of designing and constructing the apparatus are determined. The primary requirements for th...
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Hauptverfasser: | , , , , |
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Format: | Tagungsbericht |
Sprache: | eng |
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Online-Zugang: | Volltext |
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Zusammenfassung: | This paper considers the development of a small descent vehicle (SA) and technology for its descent using the autorotation effect for braking in the atmosphere. The tasks that need to be solved in the process of designing and constructing the apparatus are determined. The primary requirements for the payload (PL) are formed. |
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ISSN: | 0094-243X 1551-7616 |
DOI: | 10.1063/5.0035795 |