Stability and control of electrodynamic tethers for de-orbiting applications

Acta Astronautica

Volumn 48, Issue 5-12, 2001, Pages 491-501

  Corsi, J ^a   Iess, L ^a  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

ELECTRODYNAMICS; GEOMAGNETISM; MAGNETIC FIELD EFFECTS; PLASMA DENSITY; SPACECRAFT PROPULSION; TORQUE;

ELECTRODYNAMIC TETHERS;

TETHERLINES;

EID: 0035264787     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(01)00049-2     Document Type: Conference Paper

References (10)

1. Satellite deorbiting by means of electrodynamic tethers. General concepts and requirements
2. Electrodynamic tethers for deorbiting applications
3. Space electrodynamic tether propulsion technology system considerations & future plans
4. Performance of the terminator tether™ for autonomous deorbit of LEO spacecraft
5. Bare wire anode for electrodynamic tethers
6. Dynamics of space tether systems
7. Tethers in space handbook. Third edition