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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Bibliographic Details
Main Authors: Pavlyuchenko, V., Denisov, M., Kotlovskikh, P., Mayorova, V., Minenko, V.
Format: Conference Proceeding
Language:English
Subjects:
Autorotation
Braking
Descent
Space station payloads
Online Access:Get full text
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Description
Summary: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.
ISSN:0094-243X
1551-7616
DOI:10.1063/5.0035795