Assessing the vulnerability to debris impacts of electrodynamic tethers during typical de-orbiting missions

Earth and Planetary Sciences

• Debris 100%
• Electrodynamics 100%
• Impact 66%
• Orbitals 66%
• Spacecraft 66%
• Model 33%
• Growth 33%
• Approach 33%
• Purpose 33%
• Diameter 33%
• Altitude 33%
• Gradient 33%
• Gravitation 33%
• Low Earth Orbit 33%
• University 33%
• Cost 33%
• Circular Orbit 33%
• Italy 33%

Engineering

• Double Line 33%
• Specific Work 33%
• Tether Drag 33%
• Single Line 33%