Paper information
- Paper code
- Order
10
- Room
Technical Session #17
- Title
Success Rate and Effect of using Electrodynamic Tether System for De-orbit LEO Spacecraft
- abstract
- Session
2. Modeling and Risk Analysis
- symposium
A6. SPACE DEBRIS SYMPOSIUM
- congress
IAC-09
- Type of presentation
oral
Ms. Ieyoung Kim, Kyushu University, Japan
Prof. Toshiya Hanada, Kyushu University, Japan;
Dr. Hiroshi Hirayama, Kyushu University, Japan;