1. Application of the terminator tetherTM electrodynamic drag technology to the deorbit of constellation spacecraft;Forward,1998
2. Comparison of technologies for deorbiting spacecraft from low-earth-orbit at end of mission;Sánchez-Arriaga;Acta Astronaut.,2017
3. Mass ratio of electrodynamic tether to spacecraft on deorbit stability and efficiency;Wang;J. Guidance,2016
4. Propulsion and Power Harvesting Performance of Electrodynamic Tethers, AIAA SPACE 2011 Conference & Exposition;Hoyt,2011
5. Study on electrodynamic tether system for space debris removal;Ishige;Acta Astronaut.,2004