Deployment of a tethered satellite under the action of a braking force

Citation
G. Wiedermann et al., Deployment of a tethered satellite under the action of a braking force, Z ANG MA ME, 80, 2000, pp. S853-S854
Citations number
6
Categorie Soggetti
Mechanical Engineering
Journal title
ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK
ISSN journal
00442267 → ACNP
Volume
80
Year of publication
2000
Supplement
3
Pages
S853 - S854
Database
ISI
SICI code
0044-2267(2000)80:<S853:DOATSU>2.0.ZU;2-M
Abstract
Force braked deployment for a system of two satellites in orbit around the earth connected by a thin tether is simulated by means of a Finite Element analysis following the approach proposed in [5].