Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
5472237 | Acta Astronautica | 2017 | 22 Pages |
Abstract
The radius of perigee of the re-entry capsule cannot be considered as a single indicator of efficiency of the tether deployment control law. The set of thermal and mechanical constraints must be taken into consideration at the stages of the tether control law and the re-entry capsule design developing.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Vladimir S. Aslanov, Alexander S. Ledkov,